Defence and Strategic Goods List Amendment 2010

I, John Faulkner, Minister for Defence, make this instrument under paragraph 112 (2A) (aa) of the Customs Act 1901.

Dated 21 April 2010

JOHN FAULKNER

Minister for Defence

1 Name of instrument

  This instrument is the Defence and Strategic Goods List Amendment 2010.

2 Commencement

  This instrument commences on the day after it is registered on the Federal Register of Legislative Instruments.

3 Amendment of Defence and Strategic Goods List

  For paragraph 112 (2A) (aa) of the Customs Act 1901, the Defence and Strategic Goods List, mentioned in regulation 13E of the Customs (Prohibited Exports) Regulations 1958, is amended as set out in Schedule 1.

Note   Under regulation 13E of the Customs (Prohibited Exports) Regulations 1958, the Defence and Strategic Goods List is recognised as part of Australia’s export controls.

Schedule 1 Amendment of Defence and Strategic Goods List

(section 3)

[1] Defence and Strategic Goods List

substitute

 

 

 

 

 

 

DEFENCE AND STRATEGIC GOODS LIST

 

 

PREFACE

 

 

 

The Defence and Strategic Goods List (DSGL) is identified in regulation 13E of the Customs (Prohibited Exports) Regulations 1958 as the document titled ‘Defence and Strategic Goods List’:

(a)   formulated and published for the purpose of paragraph 112 (2A) (aa) of the Customs Act 1901 by the Minister for Defence; and

(b)   dated November 1996;

as amended by the Minister for Defence and in force from time to time.

 

Goods included in the list may not be exported from Australia unless a licence or permission has been granted by the Minister or an authorised person and that licence or permission is produced to a Collector of Customs before exportation: regulation 13E of the Customs (Prohibited Exports) Regulations 1958.

 

The DSGL was first published in 1996 when the Customs (Prohibited Exports) Regulations were consolidated and revised as a result of an Australian National Audit Office review of the Defence export control activity.

 

The DSGL includes equipment, assemblies and components, associated test, inspection and production equipment, materials, software and technology and is divided into two parts.

 

PART 1 covers defence and related goods — those goods and technologies designed or adapted for use by armed forces or goods that are inherently lethal.  These goods include:

 

 Military Goods — those goods or technology that is designed or adapted for military purposes including parts and accessories thereof.

 

 Non Military Lethal Goods (NMLG) — that equipment that is inherently lethal, incapacitating or destructive such as nonmilitary firearms, nonmilitary ammunition and commercial explosives and initiators.

 

PART 2 covers those goods that have a dual use. Dualuse goods comprise equipment and technologies developed to meet commercial needs but which may be used either as military components or for the development or production of military systems or weapons of mass destruction.  This part is further subdivided into and is made up of the following 10 categories:

 

 Category 0 — Nuclear Materials;

 Category 1 — Materials, Chemicals, Microorganisms and Toxins;

 Category 2 — Materials Processing;

 Category 3 — Electronics;

 Category 4 — Computers;

 Category 5 — Telecommunications and Information Security;

 Category 6 — Sensors and Lasers;

 Category 7 — Navigation and Avionics;

 Category 8 — Marine;

 Category 9 — Aerospace and Propulsion.

 

The DSGL is amended from time to time to reflect changes in the various multilateral nonproliferation and export control regimes of which Australia is a member.

 


 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

INTENTIONALLY BLANK

 


NOTES

 

 

1. The Notes, Technical Notes and Nota Bene (N.B.) appearing in the Defence and Strategic Goods List form an integral part of the control text.

 

2.                   The index at the end of the Defence and Strategic Goods List is provided for guidance only and does not form part of the control text.

 

3.                   The object of the controls contained in the Defence and Strategic Goods List should not be defeated by the export of any noncontrolled goods (including plant) containing one or more controlled components when the controlled component or components are the principal element of the goods and can feasibly be removed or used for other purposes.

N.B.: In judging whether the controlled component or components are to be considered the principal element, it is necessary to weigh the factors of quantity, value and technological knowhow involved and other special circumstances which might establish the controlled component or components as the principal element of the goods being procured.

 

4.                   Goods specified in the Defence and Strategic Goods List include both new and used goods.

 

5.                   Terms in “quotations” are defined terms. Refer to the “Definitions of Terms” section of the Defence and Strategic Goods List. Words and terms appearing under “Definitions of Terms”, if used in their undefined forms, take their common or dictionary meanings.

 

 

ML 8

 

Specially formulated pharmaceutical products containing ML8 materials are not controlled.

 

ML 10

 

Absence of items from the Munitions List and absence of configuration for military use would mean that an aircraft would not be considered military.

 


 

General Technology Note

 

The transfer of “technology” according to the General Technology Note, for “production” or “development” of items on this list shall be treated with vigilance.

 

General Technology Note

 

Controls on intangible “technology” are to be exercised as far as the scope of legislation† will allow.

 

General Software Note

 

The transfer of “software”, for “production” or “development” of items on this list shall be treated with vigilance in accordance with national policies and the aims of this regime.

 

Source Code

 

Taking into account national practices and legislation†, Participating States agree that “source code” items are controlled either by “software” or by “software” and “technology” controls, except when such “source code” items are explicitly decontrolled.

 

Medical equipment

 

Equipment specially designed for medical enduse that incorporates an item controlled in the DualUse List is not controlled.

 

Category 9

 

“Development” or “production” “technology” controlled by 9E for gas turbine engines remains controlled when the “technology” is used for repair, rebuild and overhaul. Excluded from control are: technical data, drawings or documentation for maintenance activities directly associated with calibration, removal or replacement of damaged or unserviceable line replaceable units, including replacement of whole engines or engine modules.

 

 

 Australia’s export control legislation on the intangible transfers of “software” and “technology” is the Weapons of Mass Destruction (Prevention of Proliferation) Act 1995. The object of this Act is to ensure that goods are not supplied or exported, and services are not provided, in circumstances where the goods will or may be used in, or the services will or may assist a Weapons of Mass Destruction (WMD) program.

 

A WMD program means a plan or program for the development, production, acquisition or stockpiling of nuclear, biological or chemical weapons or missiles capable of delivering such weapons.

 

The provision of services includes doing anything that confers a benefit on, grants a right or privilege to, provides a facility for, or otherwise assists, someone.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

INTENTIONALLY BLANK

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


 

DEFINITIONS OF TERMS

 

 

Definitions of terms between ‘single quotation marks’ are given in a Technical Note to the relevant item.

 

Definitions of terms between “double quotation marks” are as follows:

 

N.B.: Category references are given in brackets after the defined term.

 

“Accuracy” (2 6), usually measured in terms of inaccuracy, means the maximum deviation, positive or negative, of an indicated value from an accepted standard or true value.

 

“Active flight control systems” (7) are systems that function to prevent undesirable “aircraft” and missile motions or structural loads by autonomously processing outputs from multiple sensors and then providing necessary preventive commands to effect automatic control.

 

“Active pixel” (6 8) is a minimum (single) element of the solid state array which has a photoelectric transfer function when exposed to light (electromagnetic) radiation.

 

“Adapted for use in war” (1 ML7) means any modification or selection (such as altering purity, shelf life, virulence, dissemination characteristics, or resistance to UV radiation) designed to increase the effectiveness in producing casualties in humans or animals, degrading equipment or damaging crops or the environment.

 

“Adjusted Peak Performance” (4) is an adjusted peak rate at which “digital computers” perform 64bit or larger floating point additions and multiplications, and is expressed in Weighted TeraFLOPS (WT) with units of 1012 adjusted floating point operations per second.

N.B.: See Category 4, Technical Note.

 

Additives (ML8) means substances used in explosive formulations to improve their properties.

 

“Aircraft” (1 7 9 ML8 ML9 ML10) means a fixed wing, swivel wing, rotary wing (helicopter), tilt rotor or tiltwing airborne vehicle.

N.B.: See also “civil aircraft”.

 

“All compensations available” (2) means after all feasible measures available to the manufacturer to minimise all systematic positioning errors for the particular machinetool model are considered.

 

“Allocated by the ITU” (3 5) means the allocation of frequency bands according to the current edition of the ITU Radio Regulations for primary, permitted and secondary services.

N.B.: Additional and alternative allocations are not included.

 

“Angle random walk” (7) means the angular error build up with time that is due to white noise in angular rate. (IEEE STD 5282001)


“Angular position deviation” (2) means the maximum difference between angular position and the actual, very accurately measured angular position after the workpiece mount of the table has been turned out of its initial position (Reference: VDI/VDE 2617, Draft: ‘Rotary tables on coordinate measuring machines’).

 

“APP” (4) is equivalent to “Adjusted Peak Performance”.

 

“Asymmetric algorithm “ (5) means a cryptographic algorithm using different, mathematicallyrelated keys for encryption and decryption.

N.B.: A common use of “asymmetric algorithms” is key management.

 

“Automatic target tracking” (6) means a processing technique that automatically determines and provides as output an extrapolated value of the most probable position of the target in real time.

 

“Average output power” (6) means the total “laser” output energy in joules divided by the “laser duration” in seconds.

 

“Basic gate propagation delay time” (3) means the propagation delay time value corresponding to the basic gate used in a “monolithic integrated circuit”.  For a ‘family’ of “monolithic integrated circuits”, this may be specified either as the propagation delay time per typical gate within the given ‘family’ or as the typical propagation delay time per gate within the given ‘family’.

Technical Notes:

1. “Basic gate propagation delay time” is not to be confused with the input/output delay time of a complex “monolithic integrated circuit”.

2. ‘Family’ consists of all integrated circuits to which all of the following are applied as their manufacturing methodology and specifications except their respective functions:

 a. The common hardware and software architecture;

 b. The common design and process technology; and

 c. The common basic characteristics.

 

“Basic scientific research” (GTN NTN) means experimental or theoretical work undertaken principally to acquire new knowledge of the fundamental principles of phenomena or observable facts, not primarily directed towards a specific practical aim or objective.

 

“Bias” (accelerometer) (7) means the average over a specified time of accelerometer output measured at specified operating conditions that has no correlation with input acceleration or rotation. “Bias” is expressed in [m/s2, g]. (IEEE STD 5282001) (Micro g equals 1x106 g).

 

“Bias” (gyro) (7) means the average over a specified time of gyro output measured at specified operating conditions that has no correlation with input rotation or acceleration.  “Bias” is typically expressed in degrees per hour (deg/hr). (IEEE STD 5282001).

 

Biocatalysts(ML7 ML22) means enzymes for specific chemical or biochemical reactions or other biological compounds which bind to and accelerate the degradation of CW agents.

 Technical Note:

  ‘Enzymes’ means “biocatalysts” for specific chemical or biochemical reactions.


Biopolymers (ML7 ML22) means biological macromolecules as follows:

a.  Enzymes for specific chemical or biochemical reactions;

b.  Antibodies, monoclonal, polyclonal or antiidiotypic;

c.  Specially designed or specially processed receptors;

 Technical Notes:

 1. ‘Antiidiotypic antibodies’ means antibodies which bind to the specific antigen binding sites of other antibodies;

 2. ‘Monoclonal antibodies’ means proteins which bind to one antigenic site and are produced by a single clone of cells;

 3.  ‘Polyclonal antibodies’ means a mixture of proteins which bind to the specific antigen and are produced by more than one clone of cells;

4.  ‘Receptors’ means biological macromolecular structures capable of binding ligands, the binding of which affects physiological functions.

“Camming” (2), or axial displacement, means axial displacement in one revolution of the main spindle measured in a plane perpendicular to the spindle faceplate, at a point next to the circumference of the spindle faceplate (Reference:  ISO 230/1 1986, paragraph 5.63).

 

“Carbon fibre preforms” (1) means an ordered arrangement of uncoated or coated fibres intended to constitute a framework of a part before the “matrix” is introduced to form a “composite”.

 

“CE” (4) is equivalent to “computing element”.

 

“CEP” (circle of equal probability) (7) is a measure of accuracy; the radius of the circle centred at the target, at a specific range, in which 50% of the payloads impact.

 

“Chemical laser” (6) means a “laser” in which the excited species is produced by the output energy from a chemical reaction.

 

“Chemical mixture” (1) means a solid, liquid or gaseous product made up of two or more components which do not react together under the conditions under which the mixture is stored.

 

“Circulationcontrolled antitorque or circulation controlled direction control systems” (7) are systems that use air blown over aerodynamic surfaces to increase or control the forces generated by the surfaces.

 

“Civil aircraft” (1 7 9 ML10) means those “aircraft” listed by designation in published airworthiness certification lists by the civil aviation authorities to fly commercial civil internal and external routes or for legitimate civil, private or business use.

N.B.: See also “aircraft”.

 

“Commingled” (1) means filament to filament blending of thermoplastic fibres and reinforcement fibres in order to produce a fibre reinforcement “matrix” mix in total fibre form.

 

“Comminution” (1) means a process to reduce a material to particles by crushing or grinding.


“Common channel signalling” (5) is a signalling method in which a single channel between exchanges conveys, by means of labelled messages, signalling information relating to a multiplicity of circuits or calls and other information such as that used for network management.

 

“Communications channel controller” (4) means the physical interface which controls the flow of synchronous or asynchronous digital information.  It is an assembly that can be integrated into computer or telecommunications equipment to provide communications access.

 

“Compensation systems” (6) consist of the primary scalar sensor, one or more reference sensors (e.g., vector magnetometers) together with software that permit reduction of rigid body rotation noise of the platform.

 

“Composite” (1 2 6 8 9) means a “matrix” and an additional phase or additional phases consisting of particles, whiskers, fibres or any combination thereof, present for a specific purpose or purposes.

 

“Compound rotary table” (2) means a table allowing the workpiece to rotate and tilt about two nonparallel axes, which can be coordinated simultaneously for “contouring control”.

 

“III/V compounds” (3) means polycrystalline or binary or complex monocrystalline products consisting of elements of groups IIIA and VA of Mendeleyev’s periodic classification table (e.g., gallium arsenide, galliumaluminium arsenide, indium phosphide).

 

“Computing element” (“CE”) (4) means the smallest computational unit that produces an arithmetic or logic result.

 

“Contouring control” (2) means two or more “numerically controlled” motions operating in accordance with instructions that specify the next required position and the required feed rates to that position.  These feed rates are varied in relation to each other so that a desired contour is generated (ref. ISO/DIS 2806 1980).

 

“Critical temperature” (1 3 6) (sometimes referred to as the transition temperature) of a specific “superconductive” material means the temperature at which the material loses all resistance to the flow of direct electrical current.

 

“Cryptography” (5) means the discipline which embodies principles, means and methods for the transformation of data in order to hide its information content, prevent its undetected modification or prevent its unauthorised use. “Cryptography” is limited to the transformation of information using one or more ‘secret parameters’ (e.g., crypto variables) or associated key management.

Technical Note:

‘Secret parameter’: a constant or key kept from the knowledge of others or shared only within a group.

 

“CW laser” (6) means a “laser” that produces a nominally constant output energy for greater than 0.25 seconds.


“DataBased Referenced Navigation” (“DBRN”) (7) Systems means systems which use various sources of previously measured geomapping data integrated to provide accurate navigation information under dynamic conditions.  Data sources include bathymetric maps, stellar maps, gravity maps, magnetic maps or 3D digital terrain maps.

 

“Deformable mirrors” (6) (also known as adaptive optic mirrors) means mirrors having:

a. A single continuous optical reflecting surface which is dynamically deformed by the application of individual torques or forces to compensate for distortions in the optical waveform incident upon the mirror; or

b. Multiple optical reflecting elements that can be individually and dynamically repositioned by the application of torques or forces to compensate for distortions in the optical waveform incident upon the mirror.

 

“Depleted uranium” (0) means uranium depleted in the isotope 235 below that occurring in nature.

 

“Development” (GTN NTN All) is related to all stages prior to serial production, such as: design, design research, design analyses, design concepts, assembly and testing of prototypes, pilot production schemes, design data, process of transforming design data into a product, configuration design, integration design, layouts.

 

“Diffusion bonding” (1 2 9) means a solid state molecular joining of at least two separate metals into a single piece with a joint strength equivalent to that of the weakest material.

 

“Digital computer” (4 5) means equipment which can, in the form of one or more discrete variables, perform all of the following:

a. Accept data;

b. Store data or instructions in fixed or alterable (writable) storage devices;

c. Process data by means of a stored sequence of instructions which is modifiable; and

d. Provide output of data.

Technical Note:

Modifications of a stored sequence of instructions include replacement of fixed storage devices, but not a physical change in wiring or interconnections.

 

“Digital transfer rate” (5) means the total bit rate of the information that is directly transferred on any type of medium.

N.B.: See also “total digital transfer rate”.

 

“Directacting hydraulic pressing” (2) means a deformation process which uses a fluidfilled flexible bladder in direct contact with the workpiece.

 

“Dynamic adaptive routing” (5) means automatic rerouting of traffic based on sensing and analysis of current actual network conditions.

N.B.: This does not include cases of routing decisions taken on predefined information.

 

“Dynamic signal analysers” (3) means “signal analysers” which use digital sampling and transformation techniques to form a Fourier spectrum display of the given waveform including amplitude and phase information.

N.B.: See also “signal analysers”.

 

“Effective gram” (1) of “special fissile material” means:

a. For plutonium isotopes and uranium233, the isotope weight in grams;

b. For uranium enriched 1 per cent or greater in the isotope uranium235, the element weight in grams multiplied by the square of its enrichment expressed as a decimal weight fraction;

c. For uranium enriched below 1 per cent in the isotope uranium235, the element weight in grams multiplied by 0.0001

 

“Electronic assembly” (2 3 4 5) means a number of electronic components (i.e., ‘circuit elements’, ‘discrete components’, integrated circuits, etc.) connected together to perform (a) specific function(s), replaceable as an entity and normally capable of being disassembled.

Technical Notes:

1. ‘Circuit element’: a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

2. ‘Discrete component’: a separately packaged ‘circuit element’ with its own external connections.

 

“Electronically steerable phased array antenna” (5 6) means an antenna which forms a beam by means of phase coupling, (i.e., the beam direction is controlled by the complex excitation coefficients of the radiating elements) and the direction of that beam can be varied (both in transmission and reception) in azimuth or in elevation, or both, by application of an electrical signal.

 

“Endeffectors” (2 ML17) means grippers, ‘active tooling units’ and any other tooling that is attached to the baseplate on the end of a “robot” manipulator arm.

Technical Note:

‘Active tooling units’ are devices for applying motive power, process energy or sensing to the workpiece.

 

“Energetic materials” (ML 4 ML8 ML908 ML909) mean substances or mixtures that react chemically to release energy required for their intended application. “Explosives”, “pyrotechnics” and “propellants” are subclasses of energetic materials.

 

“Equivalent Density” (6) means the mass of an optic per unit optical area projected onto the optical surface.

 

“Expert systems” (7) mean systems providing results by application of rules to data which are stored independently of the “program” and capable of any of the following:

a. Modifying automatically the “source code” introduced by the user;

b. Providing knowledge linked to a class of problems in quasinatural language; or

c. Acquiring the knowledge required for their development (symbolic training).

 

“Explosives” (ML8 ML18 ML909) mean solid, liquid or gaseous substances or mixtures of substances which, in their application as primary, booster, or main charges in warheads, demolition and other applications, are required to detonate.

 

“Expression Vectors” (ML7) mean carriers (e.g., plasmid or virus) used to introduce genetic material into host cells.

 

“FADEC” is equivalent to “full authority digital engine control”.

 

“Fault tolerance” (4) is the capability of a computer system, after any malfunction of any of its hardware or “software” components, to continue to operate without human intervention, at a given level of service that provides: continuity of operation, data integrity and recovery of service within a given time.

 

“Fibrous or filamentary materials” (0 1 2 8) include:

a. Continuous “monofilaments”;

b. Continuous “yarns” and “rovings”;

c. “Tapes”, fabrics, random mats and braids;

d. Chopped fibres, staple fibres and coherent fibre blankets;

e. Whiskers, either monocrystalline or polycrystalline, of any length;

f. Aromatic polyamide pulp.

 

“Film type integrated circuit” (3) means an array of ‘circuit elements’ and metallic interconnections formed by deposition of a thick or thin film on an insulating “substrate”.

Technical Note:

‘Circuit element’ is a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

 

First generation image intensifier tubes (ML15) means electrostatically focused tubes, employing input and output fibre optic or glass face plates, multialkali photocathodes (S20 or S25), but not microchannel plate amplifiers.

 

“Fixed” (5) means that the coding or compression algorithm cannot accept externally supplied parameters (e.g., cryptographic or key variables) and cannot be modified by the user.

 

“Flight control optical sensor array” (7) is a network of distributed optical sensors, using “laser” beams, to provide realtime flight control data for onboard processing.

 

“Flight path optimisation” (7) is a procedure that minimises deviations from a fourdimensional (space and time) desired trajectory based on maximising performance or effectiveness for mission tasks.

 

“Focal plane array” (6) means a linear or twodimensional planar layer, or combination of planar layers, of individual detector elements, with or without readout electronics, which work in the focal plane.

Note: This definition does not include a stack of single detector elements or any two, three or four element detectors provided time delay and integration is not performed within the element.

 

“Fractional bandwidth” (3) means the “instantaneous bandwidth” divided by the centre frequency, expressed as a percentage.


“Frequency hopping” (5) means a form of “spread spectrum” in which the transmission frequency of a single communication channel is made to change by a random or pseudorandom sequence of discrete steps.

 

 

“Frequency switching time” (3 5) means the maximum time (i.e., delay), taken by a signal, when switched from one selected output frequency to another selected output frequency, to reach:

a. A frequency within 100 Hz of the final frequency; or

b. An output level within 1 dB of the final output level.

 

“Frequency synthesiser” (3) means any kind of frequency source or signal generator, regardless of the actual technique used, providing a multiplicity of simultaneous or alternative output frequencies, from one or more outputs, controlled by, derived from or disciplined by a lesser number of standard (or master) frequencies.

 

“Full Authority Digital Engine Control” (“FADEC”) (7 9) means an electronic control system for gas turbine or combined cycle engines utilising a digital computer to control the variables required to regulate engine thrust or shaft power output throughout the engine operating range from the beginning of fuel metering to fuel shutoff.

 

“Gas Atomisation” (1) means a process to reduce a molten stream of metal alloy to droplets of 500 µm diameter or less by a high pressure gas stream.

 

“Geographically dispersed” (6) Sensors are considered “geographically dispersed” when each location is distant from any other more than 1,500 m in any direction.  Mobile sensors are always considered “geographically dispersed”.

 

“Guidance set” (7) means systems that integrate the process of measuring and computing a vehicle’s position and velocity (i.e. navigation) with that of computing and sending commands to the vehicle’s flight control systems to correct the trajectory.

 

“Hot isostatic densification” (2) means the process of pressurising a casting at temperatures exceeding 375 K (102°C) in a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal force in all directions to reduce or eliminate internal voids in the casting.

 

“Hybrid computer” (4) means equipment which can perform all of the following:

a. Accept data;

b. Process data, in both analogue and digital representations; and

c. Provide output of data.

 

“Hybrid integrated circuit” (3) means any combination of integrated circuit(s), or integrated circuit with ‘circuit elements’ or ‘discrete components’ connected together to perform (a) specific function(s), and having all of the following characteristics:

a. Containing at least one unencapsulated device;

b. Connected together using typical IC production methods;

c. Replaceable as an entity; and

d. Not normally capable of being disassembled.

Technical Notes:

1. ‘Circuit element’: a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

2. ‘Discrete component’: a separately packaged ‘circuit element’ with its own external connections.

 

 

“Image enhancement” (4) means the processing of externally derived informationbearing images by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform).  This does not include algorithms using only linear or rotational transformation of a single image, such as translation, feature extraction, registration or false coloration.

 

“Immunotoxin” (1) is a conjugate of one cell specific monoclonal antibody and a “toxin” or “subunit of toxin”, that selectively affects diseased cells.

 

“In the public domain” (GTN NTN GSN ML22), as it applies herein, means “technology” or “software” which has been made available without restrictions upon its further dissemination (copyright restrictions do not remove “technology” or “software” from being “in the public domain”).

 

“Information security” (4 5) is all the means and functions ensuring the accessibility, confidentiality or integrity of information or communications, excluding the means and functions intended to safeguard against malfunctions.  This includes “cryptography”, ‘cryptanalysis’, protection against compromising emanations and computer security.

Technical Note:

‘Cryptanalysis’ is the analysis of a cryptographic system or its inputs and outputs to derive confidential variables or sensitive data, including clear text.

 

“Instantaneous bandwidth” (3 5 7) means the bandwidth over which output power remains constant within 3 dB without adjustment of other operating parameters.

 

“Instrumented range” (6) means the specified unambiguous display range of a radar.

 

“Insulation” (9) is applied to the components of a rocket motor, i.e. the case, nozzle, inlets, case closures, and includes cured or semicured compounded rubber sheet stock containing an insulating or refractory material.  It may also be incorporated as stress relief boots or flaps.

 

“Interconnected radar sensors” (6) means two or more radar sensors are interconnected when they mutually exchange data in real time.

 

“Interior lining” (9) is suited for the bond interface between the solid propellant and the case or insulating liner.  Usually a liquid polymer based dispersion of refractory or insulating materials, e.g. carbon filled hydroxyl terminated polybutadiene (HTPB) or other polymer with added curing agents sprayed or screeded over a case interior.

 

“Intrinsic Magnetic Gradiometer” (6) is a single magnetic field gradient sensing element and associated electronics the output of which is a measure of magnetic field gradient.

N.B.: See also “magnetic gradiometer”.

 

“Isolated live cultures” (1) includes live cultures in dormant form and in dried preparations.


 

“Isostatic presses” (2) mean equipment capable of pressurising a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal pressure in all directions within the cavity upon a workpiece or material.

 

 

“Laser” (0 2 3 5 6 7 8 9 ML5 ML9 ML19) is an assembly of components which produce both spatially and temporally coherent light that is amplified by stimulated emission of radiation.

N.B.: See also: “Chemical laser”;

   “Qswitched laser”;

   “Super High Power Laser”;

   “Transfer laser”.

 

“Laser duration” (6) means the time over which a “laser” emits “laser” radiation, which for “pulsed lasers” corresponds to the time over which a single pulse or series of consecutive pulses is emitted.

 

“Lighterthanair vehicles” (ML10) mean balloons and airships that rely on hot air or on lighterthanair gases such as helium or hydrogen for their lift.

 

“Linearity” (2) (usually measured in terms of nonlinearity) means the maximum deviation of the actual characteristic (average of upscale and downscale readings), positive or negative, from a straight line so positioned as to equalise and minimise the maximum deviations.

 

“Local area network” (4) is a data communication system having all of the following characteristics:

a. Allows an arbitrary number of independent ‘data devices’ to communicate directly with each other; and

b. Is confined to a geographical area of moderate size (e.g., office building, plant, campus, warehouse).

Technical Note:

‘Data device’ means equipment capable of transmitting or receiving sequences of digital information.

 

“Magnetic Gradiometers” (6) are instruments designed to detect the spatial variation of magnetic fields from sources external to the instrument.  They consist of multiple “magnetometers” and associated electronics the output of which is a measure of magnetic field gradient.

N.B.: See also “intrinsic magnetic gradiometer”.

 

“Magnetometers” (6) are instruments designed to detect magnetic fields from sources external to the instrument.  They consist of a single magnetic field sensing element and associated electronics the output of which is a measure of the magnetic field.

 

“Main storage” (4) means the primary storage for data or instructions for rapid access by a central processing unit.  It consists of the internal storage of a “digital computer” and any hierarchical extension thereto, such as cache storage or nonsequentially accessed extended storage.


 

“Materials resistant to corrosion by UF6” (0) may be copper, stainless steel, aluminium, aluminium oxide, aluminium alloys, nickel or alloy containing 60 weight percent or more nickel and UF6 resistant fluorinated hydrocarbon polymers, as appropriate for the type of separation process.

 

“Matrix” (1 2 8 9) means a substantially continuous phase that fills the space between particles, whiskers or fibres.

 

“Measurement uncertainty” (2) is the characteristic parameter which specifies in what range around the output value the correct value of the measurable variable lies with a confidence level of 95 %.  It includes the uncorrected systematic deviations, the uncorrected backlash and the random deviations (Reference: ISO 103602, or VDI/VDE 2617).

 

“Mechanical Alloying” (1) means an alloying process resulting from the bonding, fracturing and rebonding of elemental and master alloy powders by mechanical impact.  Nonmetallic particles may be incorporated in the alloy by addition of the appropriate powders.

 

“Melt Extraction” (1) means a process to ‘solidify rapidly’ and extract a ribbonlike alloy product by the insertion of a short segment of a rotating chilled block into a bath of a molten metal alloy.

N.B.: ‘Solidify rapidly’ means solidification of molten material at cooling rates exceeding 1,000 K/s.

 

“Melt Spinning” (1) means a process to ‘solidify rapidly’ a molten metal stream impinging upon a rotating chilled block, forming a flake, ribbon or rodlike product.

N.B.: ‘Solidify rapidly’ means solidification of molten material at cooling rates exceeding 1,000 K/s.

 

“Microcomputer microcircuit” (3) means a “monolithic integrated circuit” or “multichip integrated circuit” containing an arithmetic logic unit (ALU) capable of executing general purpose instructions from an internal storage, on data contained in the internal storage.

Technical Note:

The internal storage may be augmented by an external storage.

 

“Microprocessor microcircuit” (3) means a “monolithic integrated circuit” or “multichip integrated circuit” containing an arithmetic logic unit (ALU) capable of executing a series of general purpose instructions from an external storage.

Technical Note:

The “microprocessor microcircuit” normally does not contain integral useraccessible storage, although storage present onthechip may be used in performing its logic function.

Note: This definition includes chip sets which are designed to operate together to provide the function of a “microprocessor microcircuit”.

 

“Microorganisms” (1 2) means bacteria, viruses, mycoplasms, rickettsiae, chlamydiae or fungi, whether natural, enhanced or modified, either in the form of isolated live cultures or as material including living material which has been deliberately inoculated or contaminated with such cultures.

 

“Missiles” (1 3 6 7 9) means complete rocket systems and unmanned aerial vehicle systems, capable of delivering at least 500 kg payload to a range of at least 300 km.

 

“Monofilament” (1) or filament is the smallest increment of fibre, usually several micrometres in diameter.

 

“Monolithic integrated circuit” (3) means a combination of passive or active ‘circuit elements’ or both which:

a. Are formed by means of diffusion processes, implantation processes or deposition processes in or on a single semiconducting piece of material, a socalled ‘chip’;

b. Can be considered as indivisibly associated; and

c. Perform the function(s) of a circuit.

Technical Note:

‘Circuit element’ is a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

 

“Monospectral imaging sensors” (6) are capable of acquisition of imaging data from one discrete spectral band.

 

“Multichip integrated circuit” (3) means two or more “monolithic integrated circuits” bonded to a common “substrate”.

 

“Multidatastream processing” (4) means the microprogramor equipment architecture technique which permits simultaneous processing of two or more data sequences under the control of one or more instruction sequences by means such as:

a. Single Instruction Multiple Data (SIMD) architectures such as vector   or array processors;

b. Multiple Single Instruction Multiple Data (MSIMD) architectures;

c. Multiple Instruction Multiple Data (MIMD) architectures, including those which are tightly coupled, closely coupled or loosely coupled; or

d. Structured arrays of processing elements, including systolic arrays.

Technical Note:

 ‘Microprogram’ means a sequence of elementary instructions, maintained in a special storage, the execution of which is initiated by the introduction of its reference instruction into an instruction register.

 

“Multispectral imaging sensors” (6) are capable of simultaneous or serial acquisition of imaging data from two or more discrete spectral bands.  Sensors having more than twenty discrete spectral bands are sometimes referred to as hyperspectral imaging sensors.

 

“Natural uranium” (0) means uranium containing the mixtures of isotopes occurring in nature.

 

“Network access controller” (4) means a physical interface to a distributed switching network.  It uses a common medium which operates throughout at the same “digital transfer rate” using arbitration (e.g., token or carrier sense) for transmission. Independently from any other, it selects data packets or data groups (e.g., IEEE 802) addressed to it. It is an assembly that can be integrated into computer or telecommunications equipment to provide communications access.

 

“Neural computer” (4) means a computational device designed or modified to mimic the behaviour of a neuron or a collection of neurons, i.e., a computational device which is distinguished by its hardware capability to modulate the weights and numbers of the interconnections of a multiplicity of computational components based on previous data.

 

 

“Noise level” (6) means an electrical signal given in terms of power spectral density. The relation between “noise level” expressed in peaktopeak is given by S 2 pp = 8No(f2f1), where Spp is the peaktopeak value of the signal (e.g., nanoteslas), No is the power spectral density (e.g., (nanotesla)2/Hz) and (f2f1) defines the bandwidth of interest.

 

“Nuclear reactor” (0 ML17) means the items within or attached directly to the reactor vessel, the equipment which controls the level of power in the core, and the components which normally contain, come into direct contact with or control the primary coolant of the reactor core.

 

“Numerical control” (2) means the automatic control of a process performed by a device that makes use of numeric data usually introduced as the operation is in progress (ref. ISO 2382).

 

“Object code” (9) means an equipment executable form of a convenient expression of one or more processes (“source code” (source language)) which has been converted by programming system.

 

“Optical amplification” (5), in optical communications, means an amplification technique that introduces a gain of optical signals that have been generated by a separate optical source, without conversion to electrical signals, i.e., using semiconductor optical amplifiers, optical fibre luminescent amplifiers.

 

“Optical computer” (4) means a computer designed or modified to use light to represent data and whose computational logic elements are based on directly coupled optical devices.

 

“Optical integrated circuit” (3) means a “monolithic integrated circuit” or a “hybrid integrated circuit”, containing one or more parts designed to function as a photosensor or photoemitter or to perform (an) optical or (an) electrooptical function(s).

 

“Optical switching” (5) means the routing of or switching of signals in optical form without conversion to electrical signals.

 

“Overall current density” (3) means the total number of ampereturns in the coil (i.e., the sum of the number of turns multiplied by the maximum current carried by each turn) divided by the total crosssection of the coil (comprising the superconducting filaments, the metallic matrix in which the superconducting filaments are embedded, the encapsulating material, any cooling channels, etc.).

 

“Participating State” (7 9) is a state participating in the Wassenaar Arrangement.  (See www.wassenaar.org)

 

“Peak power” (6), means the highest level of power attained in the “laser duration”.

 

“Personalized smart card” (5) means a smart card containing a microcircuit which has been programmed for a specific application and cannot be reprogrammed for any other application by the user.

 

“Power management” (7) means changing the transmitted power of the altimeter signal so that received power at the “aircraft” altitude is always at the minimum necessary to determine the altitude.

 

Precursors (ML8) means specialty chemicals used in the manufacture of military explosives.

 

“Pressure transducers” (2) are devices that convert pressure measurements into an electrical signal.

 

“Previously separated” (0 1) means the application of any process intended to increase the concentration of the controlled isotope.

 

“Primary flight control” (7) means an “aircraft” stability or manoeuvering control using force/moment generators, i.e., aerodynamic control surfaces or propulsive thrust vectoring.

 

“Principal element” (4), as it applies in Category 4, is a “principal element” when its replacement value is more than 35% of the total value of the system of which it is an element.  Element value is the price paid for the element by the manufacturer of the system, or by the system integrator.  Total value is the normal international selling price to unrelated parties at the point of manufacture or consolidation of shipment.

 

“Production” (GTN NTN All) means all production phases, such as: construction, production engineering, manufacture, integration, assembly (mounting), inspection, testing, quality assurance.

 

“Production equipment” (1 7 9) means tooling, templates, jigs, mandrels, moulds, dies, fixtures, alignment mechanisms, test equipment, other machinery and components therefor, limited to those specially designed or modified for “development” or for one or more phases of “production”.

 

“Production facilities” (7 9) means equipment and specially designed software therefor integrated into installations for “development” or for one or more phases of “production”.

 

“Program” (2 4 5 6) means a sequence of instructions to carry out a process in, or convertible into, a form executable by an electronic computer.

 

“Propellants” (ML8) Substances or mixtures that react chemically to produce large volumes of hot gases at controlled rates to perform mechanical work.

 

“Pulse compression” (6) means the coding and processing of a radar signal pulse of long time duration to one of short time duration, while maintaining the benefits of high pulse energy.

 

“Pulse duration” (6) is the duration of a “laser” pulse measured at Full Width Half Intensity (FWHI) levels.

 

“Pulsed laser” (6) means a “laser” having a “pulse duration” that is less than or equal to 0.25 seconds.

 

 

“Pyrotechnic(s)” (ML4 ML8 ML909) means mixtures of solid or liquid fuels and oxidizers which, when ignited, undergo an energetic chemical reaction at a controlled rate intended to produce specific time delays, or quantities of heat, noise, smoke, visible light or infrared radiation.  Pyrophorics are a subclass of pyrotechnics, which contain no oxidizers but ignite spontaneously on contact with air.

 

“Quantum cryptography” (5) means a family of techniques for the establishment of a shared key for “cryptography” by measuring the quantummechanical properties of a physical system (including those physical properties explicitly governed by quantum optics, quantum field theory, or quantum electrodynamics).

 

“Qswitched laser” (6) means a “laser” in which the energy is stored in the population inversion or in the optical resonator and subsequently emitted in a pulse.

 

“Radar frequency agility” (6) means any technique which changes, in a pseudorandom sequence, the carrier frequency of a pulsed radar transmitter between pulses or between groups of pulses by an amount equal to or larger than the pulse bandwidth.

 

“Radar spread spectrum” (6) means any modulation technique for spreading energy originating from a signal with a relatively narrow frequency band, over a much wider band of frequencies, by using random or pseudorandom coding.

 

“Realtime bandwidth” (2 3) for “dynamic signal analysers” is the widest frequency range which the analyser can output to display or mass storage without causing any discontinuity in the analysis of the input data.  For analysers with more than one channel, the channel configuration yielding the widest “realtime bandwidth” shall be used to make the calculation.

 

“Real time processing” (6 7) means the processing of data by a computer system providing a required level of service, as a function of available resources, within a guaranteed response time, regardless of the load of the system, when stimulated by an external event.

 

“Repeatability” (7) means the closeness of agreement among repeated measurements of the same variable under the same operating conditions when changes in conditions or nonoperating periods occur between measurements. (Reference: IEEE STD 5282001 (one sigma standard deviation)).

 

“Required” (GTN 1 9 ML22), as applied to “technology”, refers to only that portion of “technology” which is peculiarly responsible for achieving or extending the controlled performance levels, characteristics or functions.  Such “required” “technology” may be shared by different goods.

 

“Resolution” (2) means the least increment of a measuring device; on digital instruments, the least significant bit (ref. ANSI B89.1.12).

 

“Riot control agents” (ML7) mean substances which, under the expected conditions of use for riot control purposes, rapidly produce in humans sensory irritation or disabling physical effects which disappear within a short time following termination of exposure. (Tear gases are a subset of “riot control agents”.)

 

“Robot” (2 8 ML17) means a manipulation mechanism, which may be of the continuous path or of the pointtopoint variety, may use sensors, and has all the following characteristics:

a. Is multifunctional;

b. Is capable of positioning or orienting material, parts, tools or special devices through variable movements in three dimensional space;

c. Incorporates three or more closed or open loop servodevices which may include stepping motors; and

d. Has “useraccessible programmability” by means of teach/playback method or by means of an electronic computer which may be a programmable logic controller, i.e., without mechanical intervention.

Note: The above definition does not include the following devices:

 1. Manipulation mechanisms which are only manually / teleoperator controllable;

 2. Fixed sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions.  The program is mechanically limited by fixed stops, such as pins or cams. The sequence of motions and the selection of paths or angles are not variable or changeable by mechanical, electronic or electrical means;

 3. Mechanically controlled variable sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions.  The program is mechanically limited by fixed, but adjustable stops, such as pins or cams.  The sequence of motions and the selection of paths or angles are variable within the fixed program pattern. Variations or modifications of the program pattern (e.g., changes of pins or exchanges of cams) in one or more motion axes are accomplished only through mechanical operations;

 4. Nonservocontrolled variable sequence manipulation mechanisms which are automated moving devices, operating according to mechanically fixed programmed motions.  The program is variable but the sequence proceeds only by the binary signal from mechanically fixed electrical binary devices or adjustable stops;

 5. Stacker cranes defined as Cartesian coordinate manipulator systems manufactured as an integral part of a vertical array of storage bins and designed to access the contents of those bins for storage or retrieval.

 

“Rotary atomisation” (1) means a process to reduce a stream or pool of molten metal to droplets to a diameter of 500 µm or less by centrifugal force.

 

“Roving” (1) is a bundle (typically 12–120) of approximately parallel ‘strands’.

Technical Note:

‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

 

“Runout” (2) (outoftrue running) means radial displacement in one revolution of the main spindle measured in a plane perpendicular to the spindle axis at a point on the external or internal revolving surface to be tested (Reference: ISO 230/11986, paragraph 5.61).

 

“Scale factor” (gyro or accelerometer) (7) means the ratio of change in output to a change in the input intended to be measured. Scale factor is generally evaluated as the slope of the straight line that can be fitted by the method of least squares to inputoutput data obtained by varying the input cyclically over the input range.

 

“Settling time” (3) means the time required for the output to come within onehalf bit of the final value when switching between any two levels of the converter.

 

“SHPL” (6) is equivalent to “super high power laser”.

 

“Signal analysers” (3) mean apparatus capable of measuring and displaying basic properties of the singlefrequency components of multifrequency signals.

 

“Signal processing” (3 4 5 6) means the processing of externally derived informationbearing signals by algorithms such as time compression, filtering, extraction, selection, correlation, convolution or transformations between domains (e.g., fast Fourier transform or Walsh transform).

 

“Software” (GSN All) means a collection of one or more “programs” or microprograms fixed in any tangible medium of expression.

N.B.: ‘Microprogram’ means a sequence of elementary instructions, maintained in a special storage, the execution of which is initiated by the introduction of its reference instruction into an instruction register.

 

“Source code” (or source language) (4 6 7 9) is a convenient expression of one or more processes which may be turned by a programming system into equipment executable form (“object code” (or object language)).

 

“Spacecraft” (7 9) means active and passive satellites and space probes.

 

“Space qualified” (3 6) refers to products designed, manufactured and tested to meet the special electrical, mechanical or environmental requirements for use in the launch and deployment of satellites or high altitude flight systems operating at altitudes of 100 km or higher.

 

“Special fissile material” (0) means plutonium239, uranium233, “uranium enriched in the isotopes 235 or 233”, and any material containing the foregoing.

 

“Specific modulus” (0 1 9) is Young’s modulus in pascals, equivalent to N/m2 divided by specific weight in N/m3, measured at a temperature of (296 + 2) K ((23 + 2)oC) and a relative humidity of (50 + 5)%.

 

“Specific tensile strength” (0 1 9) is ultimate tensile strength in pascals, equivalent to N/m2 divided by specific weight in N/m3, measured at a temperature of (296 + 2) K ((23 + 2)oC) and a relative humidity of (50 + 5)%.

 

“Splat Quenching” (1) means a process to ‘solidify rapidly’ a molten metal stream impinging upon a chilled block, forming a flakelike product.

N.B.: ‘Solidify rapidly’ means solidification of molten material at cooling rates exceeding 1,000 K/s.

 

“Spread spectrum” (5) means the technique whereby energy in a relatively narrowband communication channel is spread over a much wider energy spectrum.

 

“Spread spectrum” radar (6) — see “Radar spread spectrum”.

 

“Stability” (7) means the standard deviation (1 sigma) of the variation of a particular parameter from its calibrated value measured under stable temperature conditions. This can be expressed as a function of time.

 

“States (not) Party to the Chemical Weapon Convention” (1) are those states for which the Convention on the Prohibition of the Development, Production, Stockpiling and Use of Chemical Weapons has (not) entered into force.  (See www.opcw.org)

 

“Substrate” (3) means a sheet of base material with or without an interconnection pattern and on which or within which ‘discrete components’ or integrated circuits or both can be located.

Technical Notes:

1. ‘Discrete component’: a separately packaged ‘circuit element’ with its own external connections.

2. ‘Circuit element’: a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

 

“Substrate blanks” (6) means monolithic compounds with dimensions suitable for the production of optical elements such as mirrors or optical windows.

 

“Subunit of toxin” (1) is a structurally and functionally discrete component of a whole “toxin”.

 

“Superalloys” (2 9) mean nickel, cobalt or ironbase alloys having strengths superior to any alloys in the AISI 300 series at temperatures over 922 K (649oC) under severe environmental and operating conditions.

 

“Superconductive” (1 3 6 8 ML18 ML20) means materials, i.e., metals, alloys or compounds, which can lose all electrical resistance, i.e., which can attain infinite electrical conductivity and carry very large electrical currents without Joule heating.

Technical Note:

The “superconductive” state of a material is individually characterised by a “critical temperature”, a critical magnetic field, which is a function of temperature, and a critical current density which is, however, a function of both magnetic field and temperature.

 

“Super High Power Laser” (“SHPL”) (6) means a “laser” capable of delivering (the total or any portion of) the output energy exceeding 1 kJ within 50 ms or having an average or CW power exceeding 20 kW.

 

“Superplastic forming” (1 2) means a deformation process using heat for metals that are normally characterised by low values of elongation (less than 20%) at the breaking point as determined at room temperature by conventional tensile strength testing, in order to achieve elongations during processing which are at least 2 times those values.

 

“Symmetric algorithm” (5) means a cryptographic algorithm using an identical key for both encryption and decryption.

Technical Note:

A common use of “symmetric algorithms” is confidentiality of data.

 

“System tracks” (6) means processed, correlated (fusion of radar target data to flight plan position) and updated aircraft flight position report available to the Air Traffic Control centre controllers.

 

“Systolic array computer” (4) means a computer where the flow and modification of the data is dynamically controllable at the logic gate level by the user.

 

“Tape” (1) is a material constructed of interlaced or unidirectional “monofilaments”, ‘strands’, “rovings”, “tows”, or “yarns”, etc., usually preimpregnated with resin.

Technical Note:

‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

 

“Technology” (GTN NTN All) means specific information necessary for the “development”, “production” or “use” of a product. This information takes the form of ‘technical data’ or ‘technical assistance’.  Controlled “technology” for the DualUse List is defined in the General Technology Note and in the DualUse List.  Controlled “technology” for the Munitions List is specified in ML22.

Technical Notes:

1. ‘Technical data’ may take forms such as blueprints, plans, diagrams, models, formulae, tables, engineering designs and specifications, manuals and instructions written or recorded on other media or devices such as disk, tape, readonly memories.

2. ‘Technical assistance’ may take forms such as instruction, skills, training, working knowledge and consulting services. ‘Technical assistance’ may involve the transfer of ‘technical data’.

 

“Tilting spindle” (2) means a toolholding spindle which alters, during the machining process, the angular position of its centre line with respect to any other axis.

 

“Time constant” (6) is the time taken from the application of a light stimulus for the current increment to reach a value of 11/e times the final value (i.e., 63% of the final value).

 

“Total control of flight” (7) means an automated control of “aircraft” state variables and flight path to meet mission objectives responding to real time changes in data regarding objectives, hazards or other “aircraft”.

 

“Total digital transfer rate” (5) means the number of bits, including line coding, overhead and so forth per unit time passing between corresponding equipment in a digital transmission system.

N.B.:  See also “digital transfer rate”.

 

“Tow” (1) is a bundle of “monofilaments”, usually approximately parallel.

 

“Toxins” (1 2) means toxins in the form of deliberately isolated preparations or mixtures, no matter how produced, other than toxins present as contaminants of other materials such as pathological specimens, crops, foodstuffs or seed stocks of “microorganisms”.

 

“Transfer laser” (6) means a “laser” in which the lasing species is excited through the transfer of energy by collision of a nonlasing atom or molecule with a lasing atom or molecule species.

 

“Tunable” (6) means the ability of a “laser” to produce a continuous output at all wavelengths over a range of several “laser” transitions.  A line selectable “laser” produces discrete wavelengths within one “laser” transition and is not considered “tunable”.

 

“Unmanned aerial vehicle” (“UAV”) (9) means any “aircraft” capable of initiating flight and sustaining controlled flight and navigation without any human presence on board.

 

“Uranium enriched in the isotopes 235 or 233” (0) means uranium containing the isotopes 235 or 233, or both, in an amount such that the abundance ratio of the sum of these isotopes to the isotope 238 is more than the ratio of the isotope 235 to the isotope 238 occurring in nature (isotopic ratio 0.71 per cent).

 

“Use” (GTN NTN 1 2 4 5 6 7 8 9 ML21 ML22) means operation, installation (including onsite installation), maintenance (checking), repair, overhaul and refurbishing.

 

“Useraccessible programmability” (6) means the facility allowing a user to insert, modify or replace “programs” by means other than:

a. A physical change in wiring or interconnections; or

b. The setting of function controls including entry of parameters.

 

“Vaccine” (1) is a medicinal product in a pharmaceutical formulation licensed by, or having marketing or clinical trial authorisation from, the regulatory authorities of either the country of manufacture or of use, which is intended to stimulate a protective immunological response in humans or animals in order to prevent disease in those to whom or to which it is administered.

 

“Vacuum Atomisation” (1) means a process to reduce a molten stream of metal to droplets of a diameter of 500 micrometre or less by the rapid evolution of a dissolved gas upon exposure to a vacuum.

 

“Variable geometry airfoils” (7) means the use of trailing edge flaps or tabs, or leading edge slats or pivoted nose droop, the position of which can be controlled in flight.

 

“Yarn” (1) is a bundle of twisted ‘strands’.

Technical Note:

‘Strand’ is a bundle of “monofilaments” (typically over 200) arranged approximately parallel.

 


ACRONYMS AND ABBREVIATIONS

 

 

An acronym or abbreviation, when used as a defined term, will be found in the ‘Definitions of Terms’ section.

 

ACRONYM OR ABBREVIATION

MEANING

ABEC

Annular Bearing Engineers Committee

AGMA

American Gear Manufacturers’ Association

AHRS

attitude and heading reference systems

AISI

American Iron and Steel Institute

ALU

arithmetic logic unit

ANSI

American National Standards Institute

ASNO

Australian Safeguards and Nonproliferation Office

ASTM

the American Society for Testing and Materials

ATC

air traffic control

AVLIS

atomic vapour laser isotope separation

C3I

command, communications, control & intelligence

CAD

computeraideddesign

CAS

Chemical Abstracts Service

CCITT

International Telegraph and Telephone Consultative Committee

CDU

control and display unit

CEP

circular error probable

CNTD

controlled nucleation thermal deposition

CRISLA

chemical reaction by isotope selective laser activation.

CVD

chemical vapour deposition

CW

chemical warfare

CW (for lasers)

continuous wave

DEW

directed energy weapon systems

DME

distance measuring equipment

DS

directionally solidified

EBPVD

electron beam physical vapour deposition

EBU

European Broadcasting Union

ECM

electrochemical machining

ECR

electron cyclotron resonance

EDM

electrical discharge machines

EEPROMS

electrically erasable programmable read only memory

EIA

Electronic Industries Association

EMC

electromagnetic compatibility

EMCDB

elastomer modified cast double based propellants

FFT

Fast Fourier Transform

GLONASS

global navigation satellite system

GNSS

global navigation satellite system

GPS

global positioning system

HBT

heterobipolar transistors

HDDR

high density digital recording

HEMT

high electron mobility transistors

ICAO

International Civil Aviation Organisation

IEC

International Electrotechnical Commission

IEEE

Institute of Electrical and Electronic Engineers

IFOV

instantaneousfieldofview

ILS

instrument landing system

IRIG

interrange instrumentation group

ISA

international standard atmosphere

ISAR

inverse synthetic aperture radar

ISO

International Organization for Standardization

ITU

International Telecommunication Union

JIS

Japanese Industrial Standard

JT

JouleThomson

LIDAR

light detection and ranging

LRU

line replaceable unit

MAC

message authentication code

Mach

ratio of speed of an object to speed of sound (after Ernst Mach)

MLIS

molecular laser isotopic separation

MLS

microwave landing systems

MOCVD

metal organic chemical vapour deposition

MPEG

Moving Picture Experts Group (ISO/IEC JTC1/SC29/WG11)

MRI

magnetic resonance imaging

MTBF

meantimebetweenfailures

MTTF

meantimetofailure

NBC

Nuclear, Biological and Chemical

NDT

nondestructive test

PAR

precision approach radar

PIN

personal identification number

ppm

parts per million

PSD

power spectral density

QAM

quadratureamplitudemodulation

RF

radio frequency

RPV

remotely piloted air vehicle

SACMA

Suppliers of Advanced Composite Materials Association

SAR

synthetic aperture radar

SC

single crystal

SLAR

sidelooking airborne radar

SMPTE

Society of Motion Picture and Television Engineers

SRA

shop replaceable assembly

SRAM

static random access memory

SRM

SACMA Recommended Methods

SSB

single sideband

SSR

secondary surveillance radar

TCSEC

trusted computer system evaluation criteria

TIR

total indicated reading

UAV

unmanned aerial vehicle

UTS

ultimate tensile strength

UV

ultraviolet

VOR

very high frequency omnidirectional range

YAG

yttrium/aluminium garnet

 

PART 1 MUNITIONS LIST

 

 

Note 1 Terms in “quotations” are defined terms. Refer to the ‘Definitions of Terms’ section.

 

Note 2 Chemicals are listed by name and CAS number. Chemicals of the same structural formula (including hydrates) are controlled regardless of name or CAS number. CAS numbers are shown to assist in identifying whether a particular chemical or mixture is controlled, irrespective of nomenclature. CAS numbers cannot be used as unique identifiers because some forms of the listed chemical have different CAS numbers, and mixtures containing a listed chemical may also have different CAS numbers.

 

 

ML1. Smoothbore weapons with a calibre of less than 20 mm, other arms and automatic weapons with a calibre of 12.7 mm (calibre 0.50 inches) or less and accessories, as follows, and specially designed components therefor:

 

 a. Rifles, carbines, revolvers, pistols, machine pistols and machine guns:

  Note ML1.a. does not control the following:

1. Muskets, rifles and carbines manufactured earlier than 1938;

2. Reproductions of muskets, rifles and carbines the originals of which were manufactured earlier than 1890;

3.         Revolvers, pistols and machine guns manufactured earlier than 1890, and their reproductions;

  N.B:. For these goods and specially designed components therefor, see Items ML901, ML903 and ML904.

 

 b. Smoothbore weapons, as follows:

 1. Smoothbore weapons specially designed for military use;

  2. Other smoothbore weapons, as follows:

                            a. Of the fully automatic type;

 b. Of the semiautomatic or pumpaction type;

 

 c. Weapons using caseless ammunition;

 

 d. Silencers, special gunmountings, clips, weapons sights and flash suppressors for arms controlled by subitems ML1.a., ML1.b. or ML1.c.

 

Note 1 ML1. does not control smoothbore weapons used for hunting or sporting purposes.  These weapons must not be specially designed for military use or of the fully automatic firing type. For these, see Item ML901.

 

Note 2 ML1. does not control firearms specially designed for dummy ammunition and which are incapable of firing any controlled ammunition. For these, see Item ML901.


ML1. continued

 

Note 3 ML1. does not control weapons using noncentre fire cased ammunition and which are not of the fully automatic firing type. For these, see Item ML901.

 

Note 4 ML1.d. does not control optical weapon sights without electronic image processing, with a magnification of 4 times or less, provided they are not specially designed or modified for military use.

 

 

ML2. Smoothbore weapons with a calibre of 20 mm or more, other weapons or armament with a calibre greater than 12.7 mm (calibre 0.50 inches), projectors and accessories, as follows, and specially designed components therefor:

 

 a. Guns, howitzers, cannon, mortars, antitank weapons, projectile launchers, military flame throwers, rifles, recoilless rifles, smoothbore weapons and signature reduction devices therefor;

  Note 1 ML2.a. includes injectors, metering devices, storage tanks and other specially designed components for use with liquid propelling charges for any of the equipment controlled by ML2.a.

 

  Note 2 ML2.a. does not control the following:

   1. Muskets, rifles and carbines manufactured earlier than 1938;

   2. Reproductions of muskets, rifles and carbines the originals of which were manufactured earlier than 1890.

 

 b. Military smoke, gas and pyrotechnic projectors or generators.

  Note ML2.b. does not control signal pistols.

 

 c. Weapons sights.

 

 

ML3. Ammunition and fuze setting devices, as follows, and specially designed components therefor:

 

 a. Ammunition for the weapons controlled by ML1., ML2. or ML12.;

 

 b. Fuze setting devices specially designed for ammunition controlled by ML3.a.

 

Note 1 Specially designed components include:

a. Metal or plastic fabrications such as primer anvils, bullet cups, cartridge links, rotating bands and munitions metal parts;

b. Safing and arming devices, fuzes, sensors and initiation devices;

c. Power supplies with high onetime operational output;

d. Combustible cases for charges;

e. Submunitions including bomblets, minelets and terminally guided projectiles.


ML3. continued

 

Note 2 ML3.a. does not control ammunition crimped without a projectile (blank star) and dummy ammunition with a pierced powder chamber. For this, and other ammunition not covered by Item ML3, see Item ML902.

 

Note 3 ML3.a. does not control cartridges specially designed for any of the following purposes:

a. Signalling;

b. Bird scaring; or

c. Lighting of gas flares at oil wells.

 

 

ML4. Bombs, torpedoes, rockets, missiles, other explosive devices and charges and related equipment and accessories, as follows, specially designed for military use, and specially designed components therefor:

N.B.: For guidance and navigation equipment, see ML11, Note 7.

 

 a. Bombs, torpedoes, grenades, smoke canisters, rockets, mines, missiles, depth charges, demolitioncharges, demolitiondevices and demolitionkits, “pyrotechnic” devices, cartridges and simulators (i.e. equipment simulating the characteristics of any of these items);

  Note ML4.a. includes:

1. Smoke grenades, fire bombs, incendiary bombs and explosive devices;

2. Missile rocket nozzles and reentry vehicle nosetips.

 

 b. Equipment having all of the following:

 1. Specially designed for military use; and

 2. Specially designed for the handling, controlling, activating, powering with onetime operational output, launching, laying, sweeping, discharging, decoying, jamming, detonating, disrupting, disposing or detecting of any of the following:

 a. Items specified by ML4.a.; or

 b. Improvised Explosive Devices (IEDs).

 

 Note 1 ML4.b. includes:

a. Mobile gas liquefying equipment capable of producing 1,000 kg or more per day of gas in liquid form;

b. Buoyant electric conducting cable suitable for sweeping magnetic mines.

 

 Note 2 ML4.b. does not apply to handheld devices limited by design solely to the detection of metal objects and incapable of distinguishing between mines and other metal objects.


ML4. continued

 

 c. Aircraft Missile Protection Systems (AMPS).

  Note ML4.c. does not apply to AMPS having all of the following:

a. Any of the following missile warning sensors:

1. Passive sensors having peak response between 100400 nm; or

2. Active pulsed Doppler missile warning sensors;

b. Countermeasures dispensing systems;

c. Flares, which exhibit both a visible signature and an infrared signature, for decoying surfacetoair missiles; and

d. Installed on “civil aircraft” and having all of the following:

1. The AMPS is only operable in a specific “civil aircraft” in which the specific AMPS is installed and for which any of the following has been issued:

a. A civil Type Certificate; or

b. An equivalent document recognised by the International Civil Aviation Organisation (ICAO);

2. The AMPS employs protection to prevent unauthorised access to “software”; and

3. The AMPS incorporates an active mechanism that forces the system not to function when it is removed from the “civil aircraft” in which it was installed.

 

 

ML5. Fire control, and related alerting and warning equipment, and related systems, test and alignment and countermeasure equipment, as follows, specially designed for military use, and specially designed components and accessories therefor:

 

 a. Weapon sights, bombing computers, gun laying equipment and weapon control systems;

 

 b. Target acquisition, designation, rangefinding, surveillance or tracking systems; detection, data fusion, recognition or identification equipment; and sensor integration equipment;

 

 c. Countermeasure equipment for items controlled by ML5.a. or ML5.b.

 

 d. Field test or alignment equipment, specially designed for items controlled by ML5.a. or ML5.b.

 

 

ML6. Ground vehicles and components, as follows:

N.B.: For guidance and navigation equipment, see ML11, Note 7.

 

 a. Ground vehicles and components therefor, specially designed or modified for military use;

Technical Note

 For the purposes of ML6.a. the term ground vehicles includes trailers.


ML6.continued

 

 b. All wheeldrive vehicles capable of offroad use which have been manufactured or fitted with materials to provide ballistic protection to level III (NIJ 0108.01, September 1985, or comparable national standard) or better.

N.B.: See also ML13.a.

 

Note 1 ML6.a. includes:

a. Tanks and other military armed vehicles and military vehicles fitted with mountings for arms or equipment for mine laying or the launching of munitions controlled under ML4;

b. Armoured vehicles;

c. Amphibious and deep water fording vehicles;

 d. Recovery vehicles and vehicles for towing or transporting ammunition or weapon systems and associated load handling equipment.

 

Note 2 Modification of a ground vehicle for military use controlled by ML6.a. entails a structural, electrical or mechanical change involving one or more specially designed military components.  Such components include:

a. Pneumatic tyre casings of a kind specially designed to be bulletproof or to run when deflated;

b. Tyre inflation pressure control systems, operated from inside a moving vehicle;

c. Armoured protection of vital parts, (e.g., fuel tanks or vehicle cabs);

d. Special reinforcements or mountings for weapons;

e. Blackout lighting.

 

Note 3 ML6. does not control civil automobiles or trucks designed or modified for transporting money or valuables, having armoured or ballistic protection.

 

ML7. Chemical or biological toxic agents, “riot control agents”, radioactive materials, related equipment, components, and materials, as follows:

 a. Biological agents and radioactive materials “adapted for use in war” to produce casualties in humans or animals, degrade equipment or damage crops or the environment;

 

 b. Chemical warfare (CW) agents including:

  1. CW nerve agents:

   a. OAlkyl (equal to or less than C10, including cycloalkyl) alkyl (Methyl, Ethyl, nPropyl or Isopropyl) phosphonofluoridates, such as:

    Sarin (GB):OIsopropyl methylphosphonofluoridate

    (CAS 107448); and

    Soman (GD):OPinacolyl methylphosphonofluoridate

    (CAS 96640);

 

   b. OAlkyl (equal to or less than C10, including cycloalkyl)

    N,Ndialkyl (Methyl, Ethyl, nPropyl or Isopropyl) phosphoramidocyanidates, such as: Tabun (GA):OEthyl

    N,Ndimethylphosphoramidocyanidate

    (CAS 77816);

 

ML7. continued

 

   c. OAlkyl (H or equal to or less than C10, including cycloalkyl)

    S2dialkyl (Methyl, Ethyl, nPropyl or Isopropyl)aminoethyl alkyl (Methyl, Ethyl, nPropyl or Isopropyl) phosphonothiolates and corresponding alkylated and protonated salts, such as:

    VX: OEthyl S2diisopropylaminoethyl methyl phosphonothiolate (CAS 50782699);

 

  2. CW vesicant agents:

   a. Sulphur mustards, such as:

    1. 2Chloroethylchloromethylsulphide (CAS 2625765);

    2. Bis(2chloroethyl) sulphide (CAS 505602);

    3. Bis(2chloroethylthio) methane (CAS 63869136);

    4. 1,2bis (2chloroethylthio) ethane (CAS 3563368);

    5. 1,3bis (2chloroethylthio) npropane (CAS 63905102);

    6. 1,4bis (2chloroethylthio) nbutane (CAS 142868937);

    7. 1,5bis (2chloroethylthio) npentane (CAS 142868948);

    8. Bis (2chloroethylthiomethyl) ether (CAS 63918901);

    9. Bis (2chloroethylthioethyl) ether (CAS 63918898);

 

   b. Lewisites, such as:

    1. 2chlorovinyldichloroarsine (CAS 541253);

    2. Tris (2chlorovinyl) arsine (CAS 40334701);

    3. Bis (2chlorovinyl) chloroarsine (CAS 40334698);

 

   c. Nitrogen mustards, such as:

    1. HN1: bis (2chloroethyl) ethylamine (CAS 538078);

    2. HN2: bis (2chloroethyl) methylamine (CAS 51752);

    3. HN3: tris (2chloroethyl) amine (CAS 555771);

 

  3. CW incapacitating agents, such as:

   a. 3Quinuclidinyl benzilate (BZ) (CAS 6581062);

 

Note 1: For exports to “States not Party to the Chemical Weapons Convention”, ML7 does not control “chemical mixtures” containing 3Quinuclindinyl benzilate (BZ) in which BZ does not constitute more than 1% by the weight of the mixture.

 

 Note 2: For exports to “States Party to the Chemical Weapons Convention”, ML7 does not control “chemical mixtures” containing 3Quinuclindinyl benzilate (BZ) in which BZ does not constitute more than 30% by the weight of the mixture.

 

  4. CW defoliants, such as:

   a. Butyl 2chloro4fluorophenoxyacetate (LNF);

   b. 2,4,5trichlorophenoxyacetic acid mixed with

    2,4dichlorophenoxyacetic acid (Agent Orange).

 

ML7. continued

 

 c. CW binary precursors and key precursors, as follows:

  1. Alkyl (Methyl, Ethyl, nPropyl or Isopropyl Phosphonyl Difluorides, such as: DF: Methyl Phosphonyldifluoride (CAS 676993);

  2. OAlkyl (H or equal to or less than C10, including cycloalkyl) O2dialkyl (Methyl, Ethyl, nPropyl or Isopropyl) aminoethyl alkyl (Methyl, Ethyl, nPropyl or Isopropyl) phosphonites and corresponding alkylated and protonated salts, such as:

   QL: OEthyl2diisopropylaminoethyl methylphosphonite

   (CAS 57856118);

  3. Chlorosarin: OIsopropyl methylphosphonochloridate

   (CAS 1445767);

  4. Chlorosoman: OPinacolyl methylphosphonochloridate

   (CAS 7040575);

 

 d. “Riot control agents”, active constituent chemicals and combinations thereof, including:

  1. Bromobenzeneacetonitrile, (Bromobenzyl cyanide) (CA)

   (CAS 5798798);

  2. [(2chlorophenyl) methylene] propanedinitrile,

   (oChlorobenzylidenemalononitrile) (CS) (CAS 2698411);

  3. 2Chloro1phenylethanone, Phenylacyl chloride

   (chloroacetophenone) (CN) (CAS 532274);

  4. Dibenz(b,f)1,4oxazephine, (CR) (CAS 257078);

  5. 10Chloro5,10dihydrophenarsazine, (Phenarsazine chloride), (Adamsite), (DM) (CAS 578949);

  6. NNonanoylmorpholine, (MPA) (CAS 5299649);

 

Note 1 ML7.d. does not control “riot control agents” individually packaged for personal self defence purposes.

 

Note 2 ML7.d. does not control active constituent chemicals, and combinations thereof identified and packaged for food production or medical purposes.

 

 e. Equipment specially designed or modified for military use, for the dissemination of any of the following and specially designed components therefor:

  1. Materials or agents controlled by ML7.a., ML7.b. or d.; or

  2. CW made up of precursors controlled by ML7.c.

 

 f. Protective and decontamination equipment, specially designed components therefor, and specially formulated chemical mixtures, as follows:

  1. Equipment, specially designed or modified for military use, for defence against materials controlled by ML7.a., ML7.b. or d. and specially designed components therefor;

  2. Equipment, specially designed or modified for military use, for the decontamination of objects contaminated with materials controlled by ML7.a. or ML7.b. and specially designed components therefor;


ML7.f. continued

 

  3. Chemical mixtures specially developed/formulated for the decontamination of objects contaminated with materials controlled by ML7.a. or ML7.b.;

  Note ML7.f.1. includes:

a. Air conditioning units specially designed or modified for nuclear, biological or chemical filtration;

b. Protective clothing.

 

N.B.: For civil gas masks, protective and decontamination equipment see also entry 1A004.

 

 g. Equipment, specially designed or modified for military use, for the detection or identification of materials controlled by ML7.a., ML7.b. or d. and specially designed components therefor;

  Note ML7.g. does not control personal radiation monitoring dosimeters.

 

 N.B.: See also entry 1A004.

 

 h. “Biopolymers” specially designed or processed for the detection or identification of CW agents controlled by ML7.b., and the cultures of specific cells used to produce them;

 

 i. “Biocatalysts” for the decontamination or degradation of CW agents, and biological systems therefor, as follows:

  1. “Biocatalysts” specially designed for the decontamination or degradation of CW agents controlled by ML7.b. resulting from directed laboratory selection or genetic manipulation of biological systems;

  2. Biological systems, as follows: “expression vectors”, viruses or cultures of cells containing the genetic information specific to the production of “biocatalysts” controlled by ML7.i.1..

 

 Note 1 ML7.b. and ML7.d. do not control:

a. Cyanogen chloride (CAS 506774);

b. Hydrocyanic acid (CAS 74908);

c. Chlorine (CAS 7782505);

d. Carbonyl chloride (phosgene) (CAS 75445);

e. Diphosgene (trichloromethylchloroformate) (CAS 503388);

f. Deleted;

g. Xylyl bromide, ortho: (CAS 89929), meta: (CAS 620133), para: (CAS 104814);

h. Benzyl bromide (CAS 100390);

i. Benzyl iodide (CAS 620053);

j. Bromo acetone (CAS 598312);

k. Cyanogen bromide (CAS 506683);

l. Bromo methylethylketone (CAS 816400);

m. Chloro acetone (CAS 78955);

n. Ethyl iodoacetate (CAS 623483);

o. Iodo acetone (CAS 3019043);

p. Chloropicrin (CAS 76062).

ML7. continued

 

Note 2 The cultures of cells and biological systems listed in ML7.h. and ML7.i.2. are exclusive and these subitems do not control cells or biological systems for civil purposes, such as agricultural, pharmaceutical, medical, veterinary, environmental, waste management, or in the food industry.

 

Note 3 The export of chemicals listed in ML7.b.1 and b.2, ML7.c.1, c.2, c.3 and c.4 in any concentration requires permission and prior consultation with ASNO.

 

Note 4  ML7 does not control “chemical mixtures” containing one or more of the chemicals specified in entries ML7.b.4, ML7.d.1, d.2, d.3, d.4, d.5 and d.6 in which no individually specified chemical constitutes more than 30% by the weight of the mixture.

 

N.B.: See also entries 1A004, 1C350, 1C351, 1C352, 1C353, 1C354 and 1C450.

 

 

ML8. “Energetic materials”, and related substances, as follows:

 

N.B.: See also entry 1C011.

 

Technical Notes:

 1. For the purposes of this entry, mixture refers to a composition of two or more substances with at least one substance being listed in the ML8 subitems.

 2. Any substance listed in the ML8 subitems is controlled by this list, even when utilized in an application other than that indicated.  (e.g., TAGN is predominantly used as an explosive but can also be used either as a fuel or an oxidizer.)

 

 a. “Explosives”, as follows, and mixtures thereof:

  1. ADNBF (aminodinitrobenzofuroxan or 7amino4,6dinitrobenzofurazane1oxide) (CAS 97096781);

  2. BNCP (cisbis (5nitrotetrazolato) tetra aminecobalt (III) perchlorate) (CAS 117412289);

  3. CL14 (diamino dinitrobenzofuroxan or 5,7diamino4,6dinitrobenzofurazane1oxide ) (CAS 117907741);

  4. CL20 (HNIW or Hexanitrohexaazaisowurtzitane) (CAS 135285904); chlathrates of CL20 (see also ML8.g.3. and g.4. for its “precursors”);

  5. CP (2(5cyanotetrazolato) penta aminecobalt (III) perchlorate)

   (CAS 70247324);

  6. DADE (1,1diamino2,2dinitroethylene, FOX7);

  7. DATB (diaminotrinitrobenzene) (CAS 1630086);

  8. DDFP (1,4dinitrodifurazanopiperazine);

  9. DDPO (2,6diamino3,5dinitropyrazine1oxide, PZO) (CAS 194486776);

  10. DIPAM (3,3diamino2,2,4,4,6,6hexanitrobiphenyl or dipicramide) (CAS 17215440);

  11. DNGU (DINGU or dinitroglycoluril) (CAS 55510048);

ML8.a. continued

 

  12. Furazans, as follows:

   a. DAAOF (diaminoazoxyfurazan);

   b. DAAzF (diaminoazofurazan) (CAS 78644903);

  13. HMX and derivatives (see also ML8.g.5. for its “precursors”), as follows:

   a. HMX (Cyclotetramethylenetetranitramine, octahydro1,3,5,7tetranitro1,3,5,7tetrazine, 1,3,5,7tetranitro1,3,5,7tetrazacyclooctane, octogen or octogene) (CAS 2691410);

   b. difluoroaminated analogs of HMX;

   c. K55 (2,4,6,8tetranitro2,4,6,8tetraazabicyclo [3,3,0]octanone3, tetranitrosemiglycouril or ketobicyclic HMX) (CAS 130256723);

  14. HNAD (hexanitroadamantane) (CAS 143850719);

  15. HNS (hexanitrostilbene) (CAS 20062220);

  16. Imidazoles, as follows:

   a. BNNII (Octahydro2,5bis(nitroimino)imidazo [4,5d]imidazole);

   b. DNI (2,4dinitroimidazole) (CAS 5213490);

   c. FDIA (1fluoro2,4dinitroimidazole);

   d. NTDNIA (N(2nitrotriazolo)2,4dinitroimidazole);

   e. PTIA (1picryl2,4,5trinitroimidazole);

  17. NTNMH (1(2nitrotriazolo)2dinitromethylene hydrazine);

  18. NTO (ONTA or 3nitro1,2,4triazol5one) (CAS 932649);

  19. Polynitrocubanes with more than four nitro groups;

  20. PYX (2,6Bis(picrylamino)3,5dinitropyridine) (CAS 38082892);

  21. RDX and derivatives, as follows:

   a. RDX (cyclotrimethylenetrinitramine, cyclonite, T4, hexahydro1,3,5trinitro1,3,5triazine, 1,3,5trinitro1,3,5triazacyclohexane, hexogen or hexogene) (CAS 121824);

   b. KetoRDX (K6 or 2,4,6trinitro2,4,6triazacyclohexanone)

    (CAS 115029351);

  22. TAGN (triaminoguanidinenitrate) (CAS 4000162);

  23. TATB (triaminotrinitrobenzene) (CAS 3058386) (see also ML8.g.7 for its “precursors”);

  24. TEDDZ (3,3,7,7tetrabis(difluoroamine) octahydro1,5dinitro1,5diazocine);

  25. Tetrazoles, as follows:

   a. NTAT (nitrotriazol aminotetrazole);

   b. NTNT (1N(2nitrotriazolo)4nitrotetrazole);

  26. Tetryl (trinitrophenylmethylnitramine) (CAS 479458);

  27. TNAD (1,4,5,8tetranitro1,4,5,8tetraazadecalin) (CAS 135877166)

   (see also ML8.g.6. for its “precursors”);

  28. TNAZ (1,3,3trinitroazetidine) (CAS 97645244)

   (see also ML8.g.2. for its “precursors”);

  29. TNGU (SORGUYL or tetranitroglycoluril) (CAS 55510037);

  30. TNP (1,4,5,8tetranitropyridazino[4,5d]pyridazine) (CAS 229176049);

  31. Triazines, as follows:

   a. DNAM (2oxy4,6dinitroaminostriazine) (CAS 19899800);

   b. NNHT (2nitroimino5nitrohexahydro1,3,5triazine) (CAS 130400134);

ML8. a. continued

 

  32. Triazoles, as follows:

   a. 5azido2nitrotriazole;

   b. ADHTDN (4amino3,5dihydrazino1,2,4triazole dinitramide)

    (CAS 1614080);

   c. ADNT (1amino3,5dinitro1,2,4triazole);

   d. BDNTA ([bisdinitrotriazole]amine);

   e. DBT (3,3dinitro5,5bi1,2,4triazole) (CAS 30003464);

   f. DNBT (dinitrobistriazole) (CAS 70890469);

   g. NTDNA (2nitrotriazole 5dinitramide) (CAS 75393849);

   h. NTDNT (1N(2nitrotriazolo) 3,5dinitrotriazole);

   i. PDNT (1picryl3,5dinitrotriazole);

   j. TACOT (tetranitrobenzotriazolobenzotriazole) (CAS 25243361);

  33. Any explosive not listed elsewhere in ML8.a. with a detonation velocity exceeding 8,700 m/s at maximum density or a detonation pressure exceeding 34 GPa (340 kbar);

  34. Other organic explosives not listed elsewhere in ML8.a. yielding detonation pressures of 25 GPa (250 kbar) or more that will remain stable at temperatures of 523K (250oC) or higher for periods of 5 minutes or longer.

 

 b. “Propellants”, as follows:

  1. Any United Nations (UN) Class 1.1 solid “propellant” with a theoretical specific impulse (under standard conditions) of more than 250 seconds for nonmetallized, or more than 270 seconds for aluminized compositions;

  2. Any UN Class 1.3 solid “propellant” with a theoretical specific impulse (under standard conditions) of more than 230 seconds for nonhalogenized, 250 seconds for nonmetallized compositions and 266 seconds for metallized compositions;

  3. “Propellants” having a force constant of more than 1,200 kJ/kg;

  4. “Propellants” that can sustain a steadystate linear burning rate of more than 38 mm/s under standard conditions (as measured in the form of an inhibited single strand) of 6.89 MPa (68.9 bar) pressure and 294K (21oC);

  5. Elastomer modified cast double base (EMCDB) “propellants” with extensibility at maximum stress of more than 5% at 233K (40oC);

  6. Any “propellant” containing substances listed in ML8.a.

 

 c. “Pyrotechnics”, fuels and related substances, as follows, and mixtures thereof:

  1. Aircraft fuels specially formulated for military purposes;

  2. Alane (aluminium hydride) (CAS 7784216);

  3. Carboranes; decaborane (CAS 17702419); pentaboranes (CAS 19624227 and 18433846) and their derivatives;

  4. Hydrazine and derivatives, as follows (see also ML8.d.8. and d.9. for oxidising hydrazine derivatives):

   a. Hydrazine (CAS 302012) in concentrations of 70% or more;

   b. Monomethyl hydrazine (CAS 60344);

   c. Symmetrical dimethyl hydrazine (CAS 540738);

   d. Unsymmetrical dimethyl hydrazine (CAS 57147);

ML8. c. continued

 

  5. Metal fuels in particle form whether spherical, atomized, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of any of the following:

   a. Metals and mixtures thereof, as follows:

1. Beryllium (CAS 7440417) in particle sizes of less than 60 µm;

2. Iron powder (CAS 7439896) with particle size of 3 µm or less produced by reduction of iron oxide with hydrogen;

   b. Mixtures, which contain any of the following:

1. Zirconium (CAS 7440677), magnesium (CAS 7439954) or alloys of these in particle sizes of less than 60 µm;

2. Boron (CAS 7440428) or boron carbide (CAS 12069328) fuels of 85% purity or higher and particle sizes of less than 60 µm;

  6. Military materials containing thickeners for hydrocarbon fuels specially formulated for use in flame throwers or incendiary munitions, such as metal stearates or palmates (e.g. octal (CAS 637127)) and M1, M2, and M3 thickeners;

  7. Perchlorates, chlorates and chromates composited with powdered metal or other high energy fuel components;

  8. Spherical aluminium powder (CAS 7429905) with a particle size of 60 µm or less, manufactured from material with an aluminium content of 99% or more;

  9. Titanium subhydride (TiHn) of stoichiometry equivalent to n= 0.651.68.

 

Note 1 Aircraft fuels controlled by ML8.c.1. are finished products, not their constituents.

Note 2 ML8.c.4.a. does not control hydrazine mixtures specially formulated for corrosion control.

Note 3 Explosives and fuels containing the metals or alloys listed in ML8.c.5. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium, or beryllium.

Note 4 ML8.c.5.b.2. does not control boron and boron carbide enriched with boron10 (20% or more of total boron10 content.)

 

 d. Oxidizers, as follows, and mixtures thereof:

  1. ADN (ammonium dinitramide or SR 12) (CAS 140456786);

  2. AP (ammonium perchlorate) (CAS 7790989);

  3. Compounds composed of fluorine and any of the following:

   a. Other halogens;

   b. Oxygen; or

   c. Nitrogen;

Note 1 ML8.d.3 does not control chlorine trifluoride.

Note 2 ML8.d.3 does not control nitrogen trifluoride in its gaseous state.

  4. DNAD (1,3dinitro1,3diazetidine) (CAS 78246067);

  5. HAN (hydroxylammonium nitrate) (CAS 13465082);

  6. HAP (hydroxylammonium perchlorate) (CAS 15588622);

  7. HNF (hydrazinium nitroformate) (CAS 20773288);

  8. Hydrazine nitrate (CAS 37836274);

  9. Hydrazine perchlorate (CAS 27978547);

 

ML8.d. continued

 

  10. Liquid oxidisers comprised of or containing inhibited red fuming nitric acid (IRFNA) (CAS 8007587);

Note ML8.d.10 does not control noninhibited fuming nitric acid.

 

 e. Binders, plasticizers, monomers, polymers, as follows:

  1. AMMO (azidomethylmethyloxetane and its polymers) (CAS 90683297) (see also ML8.g.1. for its “precursors”);

  2. BAMO (bisazidomethyloxetane and its polymers) (CAS 17607204)

   (see also ML8.g.1. for its “precursors”);

  3. BDNPA (bis (2,2dinitropropyl)acetal) (CAS 5108690);

  4. BDNPF (bis (2,2dinitropropyl)formal) (CAS 5917613);

  5. BTTN (butanetrioltrinitrate) (CAS 6659605)

   (see also ML8.g.8. for its “precursors”);

  6. Energetic monomers, plasticizers and polymers containing nitro, azido, nitrate, nitraza or difluoroamino groups specially formulated for military use;

  7. FAMAO (3difluoroaminomethyl3azidomethyl oxetane) and its polymers;

  8. FEFO (bis(2fluoro2,2dinitroethyl) formal) (CAS 17003791);

  9. FPF1 (poly2,2,3,3,4,4hexafluoropentane1,5diol formal) (CAS 376909);

  10. FPF3 (poly2,4,4,5,5,6,6heptafluoro2trifluoromethyl3oxaheptane1,7diol formal);

  11. GAP (glycidylazide polymer) (CAS 143178249) and its derivatives;

  12. HTPB (hydroxyl terminated polybutadiene) with a hydroxyl functionality equal to or greater than 2.2 and less than or equal to 2.4, a hydroxyl value of less than 0.77 meq/g, and a viscosity at 30°C of less than 47 poise (CAS 69102905);

  13. Low (less then 10,000) molecular weight, alcohol functionalised, poly(epichlorohydrin); poly(epichlorohydrindiol) and triol;

  14. NENAs (nitratoethylnitramine compounds) (CAS 17096478, 85068731, 82486837, 82486826 and 85954069);

  15. PGN (polyGLYN, polyglycidylnitrate or poly(nitratomethyl oxirane)

   (CAS 27814488);

  16. PolyNIMMO (poly nitratomethylmethyloxetane) or polyNMMO

   (poly[3Nitratomethyl3methyloxetane]) (CAS 84051810);

  17. Polynitroorthocarbonates;

  18. TVOPA (1,2,3tris[1,2bis(difluoroamino)ethoxy] propane or tris vinoxy propane adduct) (CAS 53159390).

 

 f. “Additives”, as follows:

  1. Basic copper salicylate (CAS 62320949);

  2. BHEGA (bis(2hydroxyethyl) glycolamide) (CAS 17409415);

  3. BNO (butadienenitrileoxide) (CAS 9003183);

  4. Ferrocene derivatives, as follows:

   a. Butacene (CAS 125856624);

   b. Catocene (2,2bisethylferrocenyl propane) (CAS 37206421);

   c. Ferrocene carboxylic acids;

   d. nbutylferrocene (CAS 31904297);

   e. Other adducted polymer ferrocene derivatives;

  5. Lead betaresorcylate (CAS 20936327);

  6. Lead citrate (CAS 14450603);

ML8.f. continued

 

  7. Leadcopper chelates of betaresorcylate or salicylates (CAS 68411074);

  8. Lead maleate (CAS 19136346);

  9. Lead salicylate (CAS 15748739);

  10. Lead stannate (CAS 12036316);

  11. MAPO (tris1(2methyl)aziridinyl phosphine oxide) (CAS 57396); BOBBA 8 (bis(2methyl aziridinyl) 2(2hydroxypropanoxy) propylamino phosphine oxide); and other MAPO derivatives;

  12. Methyl BAPO (bis(2methyl aziridinyl) methylamino phosphine oxide) (CAS 85068720);

  13. Nmethylpnitroaniline (CAS 100152);

  14. 3Nitraza1,5pentane diisocyanate (CAS 7406619);

  15. Organometallic coupling agents, as follows:

   a. Neopentyl[diallyl]oxy, tri[dioctyl]phosphatotitanate (CAS 103850222); also known as titanium IV, 2,2[bis 2propenolatomethyl, butanolato, tris (dioctyl) phosphato] (CAS 110438250); or LICA 12 (CAS 103850222);

   b. Titanium IV, [(2propenolato1) methyl, npropanolatomethyl] butanolato1, tris[dioctyl] pyrophosphate or KR3538;

   c. Titanium IV, [(2propenolato1)methyl, npropanolatomethyl] butanolato1, tris(dioctyl)phosphate;

  16. Polycyanodifluoroaminoethyleneoxide;

  17. Polyfunctional aziridine amides with isophthalic, trimesic (BITA or butylene imine trimesamide), isocyanuric or trimethyladipic backbone structures and 2methyl or 2ethyl substitutions on the aziridine ring;

  18. Propyleneimine (2methylaziridine) (CAS 75558);

  19. Superfine iron oxide (Fe2O3) with a specific surface area more than 250 m2/g and an average particle size of 3.0 nm or less;

  20. TEPAN (tetraethylenepentaamineacrylonitrile) (CAS 68412453); cyanoethylated polyamines and their salts;

  21. TEPANOL (tetraethylenepentaamineacrylonitrileglycidol) (CAS 68412464); cyanoethylated polyamines adducted with glycidol and their salts;

  22. TPB (triphenyl bismuth) (CAS 603338).

 

 g. “Precursors”, as follows:

  N.B.: In ML8.g. the references are to controlled Energetic Materials manufactured from these substances.

  1. BCMO (bischloromethyloxetane) (CAS 142173260)

   (see also ML8.e.1. and e.2.);

  2. Dinitroazetidinetbutyl salt (CAS 125735388) (see also ML8.a.28.);

  3. HBIW (hexabenzylhexaazaisowurtzitane) (CAS 124782156)

   (see also ML8.a.4.);

  4. TAIW (tetraacetyldibenzylhexaazaisowurtzitane) (see also ML8.a.4.);

  5. TAT (1,3,5,7 tetraacetyl1,3,5,7,tetraaza cyclooctane) (CAS 41378987) (see also ML8.a.13.);

  6. 1,4,5,8tetraazadecalin (CAS 5409427) (see also ML8.a.27.);

  7. 1,3,5trichlorobenzene (CAS 108703) (see also ML8.a.23.);


ML8.g. continued

 

  8. 1,2,4trihydroxybutane (1,2,4butanetriol) (CAS 3068006)

   (see also ML8.e.5.).

 

Note 5 For charges and devices see ML4.

 

Note 6 ML8. does not control the following substances unless they are compounded or mixed with the “energetic material” mentioned in ML8.a. or powdered metals in ML8.c.:

   a. Ammonium picrate;

   b. Black powder;

   c. Hexanitrodiphenylamine;

   d. Difluoroamine;

   e. Nitrostarch;

   f. Potassium nitrate;

   g. Tetranitronaphthalene;

   h. Trinitroanisol;

   i. Trinitronaphthalene;

   j. Trinitroxylene;

   k. Npyrrolidinone; 1methyl2pyrrolidinone;

   l. Dioctylmaleate;

   m. Ethylhexylacrylate;

   n. Triethylaluminium (TEA), trimethylaluminium (TMA), and otlher pyrophoric metal alkyls and aryls of lithium, sodium, magnesium, zinc or boron;

   o. Nitrocellulose;

   p. Nitroglycerin (or glyceroltrinitrate, trinitroglycerine) (NG);

   q. 2,4,6trinitrotoluene (TNT);

   r. Ethylenediaminedinitrate (EDDN);

   s. Pentaerythritoltetranitrate (PETN);

   t. Lead azide, normal and basic lead styphnate, and primary explosives or priming compositions containing azides or azide complexes;

   u. Triethyleneglycoldinitrate (TEGDN);

   v. 2,4,6trinitroresorcinol (styphnic acid);

   w. Diethyldiphenyl urea; dimethylidiphenyl urea; methylethyldiphenyl urea [Centralites];

   x. N,Ndiphenylurea (unsymmetrical diphenylurea);

   y. MethylN,Ndiphenylurea (methyl unsymmetrical diphenylurea);

   z. EthylN,Ndiphenylurea (ethyl unsymmetrical diphenylurea);

   aa. 2Nitrodiphenylamine (2NDPA);

   bb. 4Nitrodiphenylamine (4NDPA);

   cc. 2,2dinitropropanol;

   dd. Nitroguanidine (see entry 1C011.d).

 

N.B.: See also item ML908.

 

 

ML9. Vessels of war, special naval equipment and accessories, as follows, and components therefor, specially designed for military use:

 N.B.: For guidance and navigation equipment, see ML11, Note 7.

 

 a. Combatant vessels and vessels (surface or underwater) specially designed or modified for offensive or defensive action, whether or not converted to nonmilitary use, regardless of current state of repair or operating condition, and whether or not they contain weapon delivery systems or armour, and hulls or parts of hulls for such vessels;

 

 b. Engines and propulsion systems, as follows:

  1. Diesel engines specially designed for submarines with both of the following characteristics:

   a. A power output of 1.12 MW (1,500 hp.) or more; and

   b. A rotary speed of 700 rpm or more;

  2. Electric motors specially designed for submarines having all of the following characteristics:

   a. A power output of more than 0.75 MW (1,000 hp.);

   b. Quick reversing;

   c. Liquid cooled; and

   d. Totally enclosed;

  3. Nonmagnetic diesel engines specially designed for military use with a power output of 37.3 kW (50 hp.) or more and with a nonmagnetic content in excess of 75% of total mass;

4. Air Independent Propulsion systems specially designed for submarines;

   Technical Note

   Air Independent Propulsion’ allows a submerged submarine to operate its propulsion system, without access to atmospheric oxygen, for a longer time than the batteries would have otherwise allowed.  This does not include nuclear power.

 

 c. Underwater detection devices specially designed for military use and controls thereof;

 

 d. Submarine and torpedo nets;

 

 e. Deleted;

 

 f. Hull penetrators and connectors specially designed for military use that enable interaction with equipment external to a vessel;

  Note ML9.f. includes connectors for vessels which are of the singleconductor, multiconductor, coaxial or waveguide type, and hull penetrators for vessels, both of which are capable of remaining impervious to leakage from without and of retaining required characteristics at marine depths exceeding 100 m; and fibreoptic connectors and optical hull penetrators specially designed for “laser” beam transmission regardless of depth. It does not include ordinary propulsive shaft and hydrodynamic controlrod hull penetrators.

 

 

ML9. continued

 

 g. Silent bearings, with gas or magnetic suspension, active signature or vibration suppression controls, and equipment containing those bearings, specially designed for military use.

 

 

ML10. “Aircraft”, “lighterthanair vehicles”, unmanned airborne vehicles, aeroengines and “aircraft” equipment, related equipment and components, specially designed or modified for military use, as follows:

N.B.: For guidance and navigation equipment, see ML11, Note 7.

 

 a. Combat “aircraft” and specially designed components therefor;

 

 b. Other “aircraft” and “lighterthanair vehicles” specially designed or modified for military use, including military reconnaissance, assault, military training, transporting and airdropping troops or military equipment, logistics support, and specially designed components therefor;

 

 c. Unmanned airborne vehicles and related equipment, specially designed or modified for military use, as follows, and specially designed components therefor:

  1. Unmanned airborne vehicles including remotely piloted air vehicles (RPVs), autonomous programmable vehicles and “lighterthanair vehicles”;

  2. Associated launchers and ground support equipment;

  3. Related equipment for command and control.

 

 d. Aeroengines specially designed or modified for military use, and specially designed components therefor;

 

 e. Airborne equipment, including airborne refuelling equipment, specially designed for use with the “aircraft” controlled by ML10.a. or ML10.b. or the aeroengines controlled by ML10.d., and specially designed components therefor;

 

 f. Pressure refuellers, pressure refuelling equipment, equipment specially designed to facilitate operations in confined areas and ground equipment, developed specially for “aircraft” controlled by ML10.a. or ML10.b., or for aeroengines controlled by ML10.d.;

 

 g. Military crash helmets and protective masks and specially designed components therefor, pressurized breathing equipment and partial pressure suits for use in “aircraft”, antig suits, liquid oxygen converters used for “aircraft” or missiles, and catapults and cartridge actuated devices for emergency escape of personnel from “aircraft”;

 

 h. Parachutes and related equipment, used for combat personnel, cargo dropping or “aircraft” deceleration, as follows, and specially designed components therefor:

  1. Parachutes for:

   a. Pin point dropping of rangers;

   b. Dropping of paratroopers;

 

ML10.h. continued

 

  2. Cargo parachutes;

  3. Paragliders, drag parachutes, drogue parachutes for stabilisation and attitude control of dropping bodies, (e.g. recovery capsules, ejection seats, bombs);

  4. Drogue parachutes for use with ejection seat systems for deployment and inflation sequence regulation of emergency parachutes;

  5. Recovery parachutes for guided missiles, drones or space vehicles;

  6. Approach parachutes and landing deceleration parachutes;

  7. Other military parachutes;

  8. Equipment specially designed for high altitude parachutists (e.g., suits, special helmets, breathing systems, navigation equipment);

 

 i. Automatic piloting systems for parachuted loads; equipment specially designed or modified for military use for controlled opening jumps at any height, including oxygen equipment.

 

Note 1 ML10.b. does not control “aircraft” or variants of those “aircraft” specially designed for military use which:

a. Are not configured for military use and are not fitted with equipment or attachments specially designed or modified for military use; and

b. Have been certified for civil use by the civil aviation authority in a participating state*.

 

Note 2 ML10.d. does not control:

a. Aeroengines designed or modified for military use which have been certified by civil aviation authorities in a participating state* for use in “civil aircraft”, or specially designed components therefor;

b. Reciprocating engines or specially designed components therefor, except those specially designed for unmanned airborne vehicles.

 

Note 3 The control in ML10.b. and ML10.d. on specially designed components and related equipment for nonmilitary “aircraft” or aeroengines modified for military use applies only to those military components and to military related equipment required for the modification to military use.

 

*N.B.: In August 2008, the Participating States of the Wassenaar Arrangement are:

 Argentina, Australia, Austria, Belgium, Bulgaria, Canada, Croatia, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Ireland, Italy, Japan, Latvia, Lithuania, Luxembourg, Malta, Netherlands, New Zealand, Norway, Poland, Portugal, Republic of Korea, Romania, Russian Federation, Slovakia, Slovenia, South Africa, Spain, Sweden, Switzerland, Turkey, Ukraine, United Kingdom and United States.

 

 

ML11. Electronic equipment, not controlled elsewhere on the Munitions List, as follows, and specially designed components therefor:

 

a. Electronic equipment specially designed for military use;


ML11 continued

 

Note ML11.a. includes:

1. Electronic countermeasure and electronic countercountermeasure equipment (i.e., equipment designed to introduce extraneous or erroneous signals into radar or radio communication receivers or otherwise hinder the reception, operation or effectiveness of adversary electronic receivers including their countermeasure equipment), including jamming and counterjamming equipment;

2. Frequency agile tubes;

3. Electronic systems or equipment designed either for surveillance and monitoring of the electromagnetic spectrum for military intelligence or security purposes or for counteracting such surveillance and monitoring;

4. Underwater countermeasures, including acoustic and magnetic jamming and decoy, equipment designed to introduce extraneous or erroneous signals into sonar receivers;

5. Data processing security equipment, data security equipment and transmission and signalling line security equipment, using ciphering processes;

6. Identification, authentification and keyloader equipment and key management, manufacturing and distribution equipment;

7. Guidance and navigation equipment;

8. Digital troposcatterradio communications transmission equipment;

9. Digital demodulators specially designed for signals intelligence.

 

b. Global Navigation Satellite Systems (GNSS) jamming equipment.

 

 

ML12. High velocity kinetic energy weapon systems and related equipment, as follows, and specially designed components therefor:

 

 a. Kinetic energy weapon systems specially designed for destruction or effecting missionabort of a target;

 

 b. Specially designed test and evaluation facilities and test models, including diagnostic instrumentation and targets, for dynamic testing of kinetic energy projectiles and systems.

 

N.B.: For weapon systems using subcalibre ammunition or employing solely chemical propulsion, and ammunition therefor, see ML1. to ML4.

 

Note 1 ML12. includes the following when specially designed for kinetic energy weapon systems:

a. Launch propulsion systems capable of accelerating masses larger than 0.1 g to velocities in excess of 1.6 km/s, in single or rapid fire modes;

b. Prime power generation, electric armour, energy storage, thermal management, conditioning, switching or fuelhandling equipment; and electrical interfaces between power supply, gun and other turret electric drive functions;

 

ML12. continued

 

c. Target acquisition, tracking, fire control or damage assessment systems;

d. Homing seeker, guidance or divert propulsion (lateral acceleration) systems for projectiles.

 

Note 2 ML12. controls weapon systems using any of the following methods of propulsion:

a. Electromagnetic;

b. Electrothermal;

c. Plasma;

d. Light gas; or

e. Chemical (when used in combination with any of the above).

 

 

ML13. Armoured or protective equipment and constructions and components, as follows:

 

 a. Armoured plate as follows:

  1. Manufactured to comply with a military standard or specification; or

  2. Suitable for military use;

 

 b. Constructions of metallic or nonmetallic materials or combinations thereof specially designed to provide ballistic protection for military systems, and specially designed components therefor;

 

 c. Helmets manufactured according to military standards or specifications, or comparable national standards, and specially designed components therefor, i.e., helmet shell, liner and comfort pads;

 

 d. Body armour and protective garments manufactured according to military standards or specifications, or equivalent, and specially designed components therefor.

 

Note 1 ML13.b. includes materials specially designed to form explosive reactive armour or to construct military shelters.

 

Note 2 ML13.c. does not control conventional steel helmets, neither modified or designed to accept, nor equipped with any type of accessory device.

 

Note 3 ML13.d. does not control body armour or protective garments when accompanying their user for the user’s own personal protection.

 

Note 4 The only helmets specially designed for bomb disposal personnel that are controlled by ML13. are those specially designed for military use.

 

N.B. 1  See also entry 1A005.

 

N.B. 2 For “fibrous or filamentary materials” used in the manufacture of body armour and helmets, see entry 1C010.

 

 

ML14. Specialised equipment for military training or for simulating military scenarios, simulators specially designed for training in the use of any firearm or weapon controlled by ML1. or ML2., and specially designed components and accessories therefor.

 

Technical Note

 The term ‘specialised equipment for military training’ includes military types of attack trainers, operational flight trainers, radar target trainers, radar target generators, gunnery training devices, antisubmarine warfare trainers, flight simulators (including humanrated centrifuges for pilot/astronaut training), radar trainers, instrument flight trainers, navigation trainers, missile launch trainers, target equipment, drone “aircraft”, armament trainers, pilotless “aircraft” trainers, mobile training units and training equipment for ground military operations.

 

Note 1 ML14. includes image generating and interactive environment systems for simulators when specially designed or modified for military use.

 

Note 2 ML14. does not control equipment specially designed for training in the use of hunting or sporting weapons.

 

 

ML15. Imaging or countermeasure equipment, as follows, specially designed for military use, and specially designed components and accessories therefor:

 

 a. Recorders and image processing equipment;

 b. Cameras, photographic equipment and film processing equipment;

 c. Image intensifier equipment;

 d. Infrared or thermal imaging equipment;

 e. Imaging radar sensor equipment;

 f. Countermeasure or countercountermeasure equipment for the equipment controlled by subitems ML15.a. to ML15.e.

  Note ML15.f. includes equipment designed to degrade the operation or effectiveness of military imaging systems or to minimize such degrading effects.

 

Note 1 The term ‘specially designed components’ includes the following when specially designed for military use:

a. Infrared image converter tubes;

b. Image intensifier tubes (other than first generation);

c. Microchannel plates;

d. Lowlightlevel television camera tubes;

e. Detector arrays (including electronic interconnection or read out systems);

f. Pyroelectric television camera tubes;

g. Cooling systems for imaging systems;

h. Electrically triggered shutters of the photochromic or electrooptical type having a shutter speed of less than 100 µs, except in the case of shutters which are an essential part of a high speed camera;

i. Fibre optic image inverters;

j. Compound semiconductor photocathodes.

 

 

 

ML15. continued

 

Note 2 ML15 does not control “first generation image intensifier tubes” or equipment specially designed to incorporate “first generation image intensifier tubes”.

N.B.: For the status of weapons sights incorporating “first generation image intensifer tubes” see entries ML1.d, ML2.c and ML5.a.

 

N.B.: See also entries 6A002.a.2. and 6A002.b.

 

 

ML16. Forgings, castings and other unfinished products the use of which in a controlled product is identifiable by material composition, geometry or function, and which are specially designed for any products controlled by ML1.to ML4., ML6., ML9., ML10., ML12. or ML19.

 

 

ML17. Miscellaneous equipment, materials and libraries, as follows, and specially designed components therefor:

 

 a. Selfcontained diving and underwater swimming apparatus, as follows:

  1. Closed or semiclosed circuit (rebreathing) apparatus specially designed for military use (i.e. specially designed to be non magnetic);

  2. Specially designed components for use in the conversion of opencircuit apparatus to military use;

  3. Articles designed exclusively for military use with selfcontained diving and underwater swimming apparatus;

 

 b. Construction equipment specially designed for military use;

 

 c. Fittings, coatings and treatments for signature suppression, specially designed for military use;

 

 d. Field engineer equipment specially designed for use in a combat zone;

 

 e. “Robots”, “robot” controllers and “robot” “endeffectors”, having any of the following characteristics:

  1. Specially designed for military use;

  2. Incorporating means of protecting hydraulic lines against externally induced punctures caused by ballistic fragments (e.g., incorporating selfsealing lines) and designed to use hydraulic fluids with flash points higher than 839 K (566°C); or

  3. Specially designed or rated for operating in an electromagnetic pulse (EMP) environment;

 

 f. Libraries (parametric technical databases) specially designed for military use with equipment controlled by the Munitions List;

 

 g. Nuclear power generating equipment or propulsion equipment, including “nuclear reactors”, specially designed for military use and components therefor specially designed or modified for military use;

 

 h. Equipment and material, coated or treated for signature suppression, specially designed for military use, other than those controlled elsewhere in the Munitions List;

 

 i. Simulators specially designed for military “nuclear reactors”;

ML17. continued

 

 j. Mobile repair shops specially designed or modified to service military equipment;

 

 k. Field generators specially designed or modified for military use;

 

 l. Containers specially designed or modified for military use;

 

 m. Ferries, other than those controlled elsewhere in the Munitions List, bridges and pontoons, specially designed for military use;

 

 n. Test models specially designed for the “development” of items controlled by ML4., ML6., ML9. or ML10.;

 

 o. Laser protection equipment (e.g., eye and sensor protection) specially designed for military use.

 

Technical Notes

 1. For the purpose of ML17, the term ‘library’ (parametric technical database) means a collection of technical information of a military nature, reference to which may enhance the performance of military equipment or systems.

 2. For the purpose of ML17, ‘modified’ means any structural, electrical, mechanical, or other change that provides a nonmilitary item with military capabilities equivalent to an item which is specially designed for military use.

 

 

ML18. Equipment for the production of products referred to in the Munitions List, as follows:

 

 a. Specially designed or modified production equipment for the production of products controlled by the Munitions List, and specially designed components therefor;

 

 b. Specially designed environmental test facilities and specially designed equipment therefor, for the certification, qualification or testing of products controlled by the Munitions List.

 

Technical Note

For the purposes of ML18., the term ‘production’ includes design, examination, manufacture, testing and checking.

 

Note ML18.a. and ML18.b. include the following equipment:

a. Continuous nitrators;

b. Centrifugal testing apparatus or equipment having any of the following characteristics:

1. Driven by a motor or motors having a total rated horsepower of more than 298 kW (400 hp);

2. Capable of carrying a payload of 113 kg or more; or

3. Capable of exerting a centrifugal acceleration of 8 g or more on a payload of 91 kg or more;

c. Dehydration presses;

d. Screw extruders specially designed or modified for military explosive extrusion;

e. Cutting machines for the sizing of extruded propellants;

 

ML18. continued

 

f. Sweetie barrels (tumblers) 1.85 m or more in diameter and having over 227 kg product capacity;

g. Continuous mixers for solid propellants;

h. Fluid energy mills for grinding or milling the ingredients of military explosives;

i. Equipment to achieve both sphericity and uniform particle size in metal powder listed in ML8.c.8.;

j. Convection current converters for the conversion of materials listed in ML8.c.3.

 

 

ML19. Directed energy weapon systems (DEW), related or countermeasure equipment and test models, as follows, and specially designed components therefor:

 

 a. “Laser” systems specially designed for destruction or effecting missionabort of a target;

 

 b. Particle beam systems capable of destruction or effecting missionabort of a target;

 

 c. High power radiofrequency (RF) systems capable of destruction or effecting missionabort of a target;

 

 d. Equipment specially designed for the detection or identification of, or defence against, systems controlled by ML19.a. to ML19.c.;

 

 e. Physical test models for the systems, equipment and components controlled by this Item;

 

 f. Continuous wave or pulsed “laser” systems specially designed to cause permanent blindness to unenhanced vision, i.e., to the naked eye or to the eye with corrective eyesight devices.

 

Note 1 Directed energy weapon systems controlled by ML19. include systems whose capability is derived from the controlled application of:

a. “Lasers” of sufficient continuous wave or pulsed power to effect destruction similar to the manner of conventional ammunition;

b. Particle accelerators which project a charged or neutral particle beam with destructive power;

c. High pulsed power or high average power radio frequency beam transmitters which produce fields sufficiently intense to disable electronic circuitry at a distant target.

 

Note 2 ML19. includes the following when specially designed for directed energy weapon systems:

a. Prime power generation, energy storage, switching, power conditioning or fuelhandling equipment;

b. Target acquisition or tracking systems;


ML19. continued

 

c. Systems capable of assessing target damage, destruction or missionabort;

d. Beamhandling, propagation or pointing equipment;

e. Equipment with rapid beam slew capability for rapid multiple target operations;

f. Adaptive optics and phase conjugators;

g. Current injectors for negative hydrogen ion beams;

h. “Space qualified” accelerator components;

i. Negative ion beam funnelling equipment;

j. Equipment for controlling and slewing a high energy ion beam;

k. “Space qualified” foils for neutralising negative hydrogen isotope beams.

 

 

ML20. Cryogenic and “superconductive” equipment, as follows, and specially designed components and accessories therefor:

 

 a. Equipment specially designed or configured to be installed in a vehicle for military ground, marine, airborne or space applications, capable of operating while in motion and of producing or maintaining temperatures below 103 K (170°C);

  Note ML20.a. includes mobile systems incorporating or employing accessories or components manufactured from nonmetallic or nonelectrical conductive materials, such as plastics or epoxyimpregnated materials.

 

 b. “Superconductive” electrical equipment (rotating machinery and transformers) specially designed or configured to be installed in a vehicle for military ground, marine, airborne or space applications, capable of operating while in motion.

  Note ML20.b. does not control directcurrent hybrid homopolar generators that have singlepole normal metal armatures which rotate in a magnetic field produced by superconducting windings, provided those windings are the only superconducting component in the generator.

 

ML21. “Software” as follows:

 

 a. “Software” specially designed or modified for the “development”, “production” or “use” of equipment, materials or “software”, specified by the Munitions List;

 

 b. Specific “software”, other than that specified by ML21.a., as follows:

  1. “Software” specially designed for military use and specially designed for modelling, simulating or evaluating military weapon systems;

 

  2. “Software” specially designed for military use and specially designed for modelling or simulating military operational scenarios;

 

  3. “Software” for determining the effects of conventional, nuclear, chemical or biological weapons;


ML.21. continued

 

  4. “Software” specially designed for Command, Communications, Control and Intelligence (C3I) or Command, Communications, Control, Computer and Intelligence (C4I) applications;

 

 c. “Software”, not specified by ML21.a., or b., specially designed or modified to enable equipment not specified by the Munitions List to perform the military functions of equipment specified by the Munitions List.

 

 

ML22. “Technology” as follows:

 

 a. “Technology”, other than specified in ML22.b, which is “required” for the “development”, “production” or “use” of items controlled in the Munitions List.

 

 b. “Technology” as follows:

  1. “Technology” “required” for the design of, the assembly of components into, and the operation, maintenance and repair of complete production installations for items controlled in the Munitions List, even if the components of such production installations are not controlled;

  2. “Technology” “required” for the “development” and “production” of small arms even if used to produce reproductions of antique small arms;

  3. “Technology” “required” for the “development”, “production” or “use” of toxicological agents, related equipment or components controlled by ML7.a. to ML7.g.;

  4. “Technology” “required” for the “development”, “production” or “use” of “biopolymers” or cultures of specific cells controlled by ML7.h.;

  5. “Technology” “required” exclusively for the incorporation of “biocatalysts”, controlled by ML7.i.1., into military carrier substances or military material.

 

Note 1 “Technology” “required” for the “development”, “production” or “use” of items controlled in the Munitions List remains under control even when applicable to any uncontrolled item.

 

Note 2 ML22 does not control “technology” as follows:

a. Which is the minimum necessary for the installation, operation, maintenance (checking) and repair of those items which are not controlled or whose export has been authorised;

b. Which is “in the public domain”, “basic scientific research” or the minimum necessary information for patent applications;

c. For magnetic induction for continuous propulsion of civil transport devices.

 

 

 

ML901. Non-military firearms including rifles, carbines, muskets, pistols, revolvers, shotguns, and smoothbore weapons, not specified in ML1, and specially designed components therefor.

 

 

ML902. Ammunition, projectiles, and specially designed components therefor, for the firearms specified in ML901.

 

Technical Note:

Specially designed components for the products controlled by ML901 and ML902 include forgings, castings and other unfinished products the use of which in a controlled product is identifiable by material composition, geometry or function.

 

ML903. Deleted.

 

ML904. Accessories, including silencers, special gunmountings, magazines, weapon sights and flash suppressors, for the firearms specified in ML901.

 

ML905. Air guns having any of the following characteristics and specially designed components therefor:

 a.              muzzle velocity exceeding 152.4 m/s (500 feet per second);

 b.              designed for competition target shooting; or

 c.              capable of fully automatic operation.

 

Technical Note:

Air guns discharge a projectile by the use of compressed air or gas and not by the explosive force of propellant combustion. Air guns include any air pistol or air rifle.

 

Note: ML905 does not include air gun accessories, air gun pellets or other air gun projectiles.

 

ML908. "Energetic materials" other than "energetic materials" specified in ML8, including high explosives specified in 1C239, but excluding those specially formulated for toys, novelty goods and fireworks.

 

ML909. Detonators or other equipment for the initiation of nonmilitary "energetic materials" specified in ML908.

 

Note:  ML901 to ML909 do not include nailing or stapling guns, explosive powered fixing tools, starting pistols, flare guns or other signalling devices designed for emergency or lifesaving purposes, line throwers, tranquilliser guns, guns that operate a captive bolt for the slaughter of animals, devices for the casting of weighted nets, underwater powerheads, fire extinguisher cartridges, hand-operated devices that use blank cartridges to propel objects for retrieval in connection with the training of dogs, paintball guns, airsoft guns (6mm or 8mm calibre), air bag and life raft inflation gas generators, thermal welding charges and associated ignition tapes, sidewall core guns designed for geological or mining purposes, expandable casing perforation guns designed for geological or mining purposes, oil well gas flare igniters, birdfright cartridges, improvised explosive device disposal (IEDD) disruptor cartridges or any other cartridges or "explosive"/"pyrotechnic" charges specially designed for use with the items listed in this Note.

 

ML910. Charges and devices containing "energetic materials" specified in ML908.

 

PART 2 – DUALUSE LIST

 

 

Note 1 Terms in “quotations” are defined terms. Refer to the ‘Definitions of Terms’ section.

 

Note 2 Chemicals are listed by name and CAS number. Chemicals of the same structural formula (including hydrates) are controlled regardless of name or CAS number. CAS numbers are shown to assist in identifying whether a particular chemical or mixture is controlled, irrespective of nomenclature. CAS numbers cannot be used as unique identifiers because some forms of the listed chemical have different CAS numbers, and mixtures containing a listed chemical may also have different CAS numbers.

 

NUCLEAR TECHNOLOGY NOTE (NTN)

 

(To be read in conjunction with section E of Category 0.)

 

1. The “technology” directly associated with any goods controlled in Category 0 is controlled according to the provisions of Category 0.

 

2. “Technology” for the “development”, “production” or “use” of goods under control remains under control even when applicable to noncontrolled goods.

 

3. The approval of goods for export also authorizes the export to the same enduser of the minimum “technology” required for the installation, operation, maintenance and repair of the goods.

 

4. Controls on “technology” transfer do not apply to information “in the public domain” or to “basic scientific research”.

 

GENERAL TECHNOLOGY NOTE (GTN)

 

(To be read in conjunction with section E of Categories 1 to 9.)

 

1. The export of “technology” which is “required” for the “development”, “production” or “use” of goods controlled in Categories 1 to 9, is controlled according to the provisions of Categories 1 to 9.

 

2.              “Technology” “required” for the “development”, “production” or “use” of goods under control remains under control even when applicable to noncontrolled goods.

 

3.              Controls do not apply to that “technology” which is the minimum necessary for the installation, operation, maintenance (checking) and repair of those goods which are not controlled or whose export has been authorised.

              N.B.: This does not release such “technology” specified in 1E002.e., 1E002.f.,  8E002.a. and 8E002.b.

 

4.              Controls on “technology” transfer do not apply to information “in the public domain”, to “basic scientific research” or to the minimum necessary information for patent applications.

 

GENERAL SOFTWARE NOTE (GSN)

 

(This note overrides any control within section D of Categories 0 to 9.)

 

Categories 0 to 9 of this list do not control “software” which is either:

 

1. Generally available to the public by being:

 a. Sold from stock at retail selling points, without restriction, by means of:

 1. Overthecounter transactions;

 2. Mail order transactions;

 3. Electronic transactions; or

 4. Telephone order transactions; and

 

 b. Designed for installation by the user without further substantial support by the supplier; or

 

N.B.: Entry a. of the General Software Note does not release “software” specified in Category 5 — Part 2 (“Information Security”).

 

2. “In the public domain”.

 

 

CATEGORY 0 NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT

 

 

0A Systems, Equipment and Components

 

0A001 “Nuclear reactors” and specially designed or prepared equipment and components therefor, as follows:

 

 a. “Nuclear reactors” capable of operation so as to maintain a controlled selfsustaining fission chain reaction;

 

 b. Metal vessels, or major shopfabricated parts therefor, specially designed or prepared to contain the core of a “nuclear reactor”, including the reactor vessel head for a reactor pressure vessel;

 

 c. Manipulative equipment specially designed or prepared for inserting or removing fuel in a “nuclear reactor”;

 

 d. Control rods specially designed or prepared for the control of the fission process in a “nuclear reactor”, support or suspension structures therefor, rod drive mechanisms and rod guide tubes;

 

 e. Pressure tubes specially designed or prepared to contain fuel elements and the primary coolant in a “nuclear reactor” at an operating pressure in excess of 5.1 MPa;

 

 f. Zirconium metal and alloys in the form of tubes or assemblies of tubes in which the ratio of hafnium to zirconium is less than 1:500 parts by weight, specially designed or prepared for use in a “nuclear reactor”;

 

 g. Coolant pumps specially designed or prepared for circulating the primary coolant of “nuclear reactors”;

 

 h. ‘Nuclear reactor internals’ specially designed or prepared for use in a “nuclear reactor”, including support columns for the core, fuel channels, thermal shields, baffles, core grid plates, and diffuser plates;

 Note: In 0A001.h. ‘nuclear reactor internals’ means any major structure within a reactor vessel which has one or more functions such as supporting the core, maintaining fuel alignment, directing primary coolant flow, providing radiation shields for the reactor vessel, and guiding incore instrumentation.

 

 i. Heat exchangers (steam generators) specially designed or prepared for use in the primary coolant circuit of a “nuclear reactor”;

 

 j. Neutron detection and measuring instruments specially designed or prepared for determining neutron flux levels within the core of a “nuclear reactor”.

 

0B Test, Inspection and Production Equipment

 

0B001 Plant for the separation of isotopes of “natural uranium”, “depleted uranium” and “special fissile materials”, and specially designed or prepared equipment and components therefor, as follows:

 

 a. Plant specially designed for separating isotopes of “natural uranium”, “depleted uranium”, and “special fissile materials”, as follows:

 

 1. Gas centrifuge separation plant;

 2. Gaseous diffusion separation plant;

 3. Aerodynamic separation plant;

 4. Chemical exchange separation plant;

 5. Ionexchange separation plant;

 6. Atomic vapour “laser” isotope separation (AVLIS) plant;

 7. Molecular “laser” isotope separation (MLIS) plant;

 8. Plasma separation plant;

 9. Electro magnetic separation plant;

 

 b. Gas centrifuges and assemblies and components, specially designed or prepared for gas centrifuge separation process, as follows:

 

 Note: In 0B001.b. ‘high strengthtodensity ratio material’ means any of the following:

  a. Maraging steel capable of an ultimate tensile strength of 2,050 MPa or more;

  b. Aluminium alloys capable of an ultimate tensile strength of 460 MPa or more; or

  c. “Fibrous or filamentary materials” with a “specific modulus” of more than 3.18 x 106 m and a “specific tensile strength” greater than 76.2 x 103 m;

 

 1. Gas centrifuges;

 

 2. Complete rotor assemblies;

 

 3. Rotor tube cylinders with a wall thickness of 12 mm or less, a diameter of between 75 mm and 400 mm, made from ‘high strengthtodensity ratio materials’;

 

 4. Rings or bellows with a wall thickness of 3 mm or less and a diameter of between 75 mm and 400 mm and designed to give local support to a rotor tube or to join a number together, made from ‘high strengthtodensity ratio materials’;

 

 5. Baffles of between 75 mm and 400 mm diameter for mounting inside a rotor tube, made from ‘high strengthtodensity ratio materials’;

 

 6. Top or bottom caps of between 75 mm and 400 mm diameter to fit the ends of a rotor tube, made from ‘high strengthtodensity ratio materials’;

0B001 b. continued

 

 7. Magnetic suspension bearings consisting of an annular magnet suspended within a housing made of or protected by “materials resistant to corrosion by UF6” containing a damping medium and having the magnet coupling with a pole piece or second magnet fitted to the top cap of the rotor;

 

 8. Specially prepared bearings comprising a pivotcup assembly mounted on a damper;

 

 9. Molecular pumps comprised of cylinders having internally machined or extruded helical grooves and internally machined bores;

 

 10. Ringshaped motor stators for multiphase AC hysteresis (or reluctance) motors for synchronous operation within a vacuum in the frequency range of 600 to 2,000 Hz and a power range of 50 to 1,000 VoltAmps;

 

 11. Centrifuge housing/recipients to contain the rotor tube assembly of a gas centrifuge, consisting of a rigid cylinder of wall thickness up to 30 mm with precision machined ends and made of or protected by “materials resistant to corrosion by UF6”;

 

 12. Scoops consisting of tubes of up to 12 mm internal diameter for the extraction of UF6 gas from within a centrifuge rotor tube by a Pitot tube action, made of or protected by “materials resistant to corrosion by UF6”;

 

 13. Frequency changers (converters or inverters) specially designed or prepared to supply motor stators for gas centrifuge enrichment, having all of the following characteristics, and specially designed components therefor:

 a. Multiphase output of 600 to 2,000 Hz;

 b. Frequency control better than 0.1%;

 c. Harmonic distortion of less than 2%; and

 d. An efficiency greater than 80%;

 

14. Bellows valves made of or protected by “materials resistant to corrosion by UF6”, with a diameter of 10 mm to 160 mm;

 

 c. Equipment and components, specially designed or prepared for gaseous diffusion separation process, as follows:

 

 1. Gaseous diffusion barriers made of porous metallic, polymer or ceramic “materials resistant to corrosion by UF6” with a pore size of 10 to 100 nm, a thickness of 5 mm or less, and, for tubular forms, a diameter of 25 mm or less;

 

 2. Gaseous diffuser housings made of or protected by “materials resistant to corrosion by UF6”;

 

0B001 c. continued

 

 3. Compressors (positive displacement, centrifugal and axial flow types) or gas blowers with a suction volume capacity of 1 m3/min or more of UF6, and discharge pressure up to 666.7 kPa, made of or protected by “materials resistant to corrosion by UF6”;

 

 4. Rotary shaft seals for compressors or blowers specified in 0B001.c.3. and designed for a buffer gas inleakage rate of less than 1,000 cm3/min.;

 

 5. Heat exchangers made of aluminium, copper, nickel, or alloys containing more than 60 per cent nickel, or combinations of these metals as clad tubes, designed to operate at subatmospheric pressure with a leak rate that limits the pressure rise to less than 10 Pa per hour under a  pressure differential of 100 kPa;

 

 6. Bellow valves made of or protected by “materials resistant to corrosion by UF6”, with a diameter of 40 mm to 1,500 mm;

 

 d. Equipment and components, specially designed or prepared for aerodynamic separation process, as follows:

 

 1. Separation nozzles consisting of slitshaped, curved channels having a radius of curvature less than 1 mm, resistant to corrosion by UF6, and having a knifeedge contained within the nozzle which separates the gas flowing through the nozzle into two streams;

 

 2. Tangential inlet flowdriven cylindrical or conical tubes, (vortex tubes), made of or protected by “materials resistant to corrosion by UF6” with a diameter of between 0.5 cm and 4 cm and a length to diameter ratio of 20:1 or less and with one or more tangential inlets;

 

 3. Compressors (positive displacement, centrifugal and axial flow types) or gas blowers with a suction volume capacity of 2 m3/min or more, made of or protected by “materials resistant to corrosion by UF6”, and rotary shaft seals therefor;

 

 4. Heat exchangers made of or protected by “materials resistant to corrosion by UF6”;

 

 5. Aerodynamic separation element housings, made of or protected by “materials resistant to corrosion by UF6” to contain vortex tubes or separation nozzles;

 

 6. Bellows valves made of or protected by “materials resistant to corrosion by UF6”, with a diameter of 40 to 1,500 mm;

0B001 d. continued

 

 7. Process systems for separating UF6 from carrier gas (hydrogen or helium) to 1 ppm UF6 content or less, including:

 a. Cryogenic heat exchangers and cryoseparators capable of temperatures of 153K (120°C) or less;

 b. Cryogenic refrigeration units capable of temperatures of 153 K (120°C) or less;

 c. Separation nozzle or vortex tube units for the separation of UF6 from carrier gas;

 d. UF6 cold traps capable of temperatures of 253 K (20°C) or less;

 

 e. Equipment and components, specially designed or prepared for chemical exchange separation process, as follows:

 

 1. Fastexchange liquidliquid pulse columns with stage residence time of 30 seconds or less and resistant to concentrated hydrochloric acid (e.g. made of or protected by suitable plastic materials such as fluorocarbon polymers or glass);

 

 2. Fastexchange liquidliquid centrifugal contactors with stage residence time of 30 seconds or less and resistant to concentrated hydrochloric acid (e.g. made of or protected by suitable plastic materials such as fluorocarbon polymers or glass);

 

 3. Electrochemical reduction cells resistant to concentrated hydrochloric acid solutions, for reduction of uranium from one valence state to another;

 

 4. Electrochemical reduction cells feed equipment to take U+4 from the organic stream and, for those parts in contact with the process stream, made of or protected by suitable materials (e.g. glass, fluorocarbon polymers, polyphenyl sulphate, polyether sulfone and resinimpregnated graphite);

 

 5. Feed preparation systems for producing high purity uranium chloride solution consisting of dissolution, solvent extraction and/or ion exchange equipment for purification and electrolytic cells for reducing the uranium U+6 or U+4 to U+3;

 

 6. Uranium oxidation systems for oxidation of U+3 to U+4;

 

 f. Equipment and components, specially designed or prepared for ionexchange separation process, as follows:

 

0B001 f. continued

 

 1. Fast reacting ionexchange resins, pellicular or porous macroreticulated resins in which the active chemical exchange groups are limited to a coating on the surface of an inactive porous support structure, and other composite structures in any suitable form, including particles or fibres, with diameters of 0.2 mm or less, resistant to concentrated hydrochloric acid and designed to have an exchange rate halftime of less than 10 seconds and capable of operating at temperatures in the range of 373 K (100oC) to 473 K (200oC);

 

 2. Ion exchange columns (cylindrical) with a diameter greater than 1,000 mm, made of or protected by materials resistant to concentrated hydrochloric acid (e.g. titanium or fluorocarbon plastics) and capable of operating at temperatures in the range of 373 K (100oC) to 473 K (200oC) and pressures above 0.7 MPa;

 

 3. Ion exchange reflux systems (chemical or electrochemical oxidation or reduction systems) for regeneration of the chemical reducing or oxidizing agents used in ion exchange enrichment cascades;

 

 g. Equipment and components, specially designed or prepared for atomic vapour “laser” isotope separation process (AVLIS), as follows:

 

 1. High power strip or scanning electron beam guns with a delivered power of more than 2.5 kW/cm for use in uranium vaporization systems;

 

 2. Liquid uranium metal handling systems for molten uranium or uranium alloys, consisting of crucibles, made of or protected by suitable corrosion and heat resistant materials (e.g. tantalum, yttriacoated graphite, graphite coated with other rare earth oxides or mixtures thereof), and cooling equipment for the crucibles;

  N.B.:    SEE ALSO 2A225.

 

 3. Product and tails collector systems made of or lined with materials resistant to the heat and corrosion of uranium metal vapour or liquid, such as yttriacoated graphite or tantalum;

 

 4. Separator module housings (cylindrical or rectangular vessels) for containing the uranium metal vapour source, the electron beam gun and the product and tails collectors;

 

 5. “Lasers” or “laser” systems for the separation of uranium isotopes with a spectrum frequency stabiliser for operation over extended periods of time;

  N.B.:     SEE ALSO 6A005 AND 6A205.

0B001 continued

 

 h. Equipment and components, specially designed or prepared for molecular “laser” isotope separation process (MLIS) or chemical reaction by isotope selective laser activation (CRISLA), as follows:

 

 1. Supersonic expansion nozzles for cooling mixtures of UF6 and carrier gas to 150 K (123°C) or less and made from “materials resistant to corrosion by UF6”;

 

 2. Uranium pentafluoride (UF5) product collectors consisting of filter, impact, or cyclonetype collectors or combinations thereof, and made of “materials resistant to corrosion by UF5/UF6”;

 

 3. Compressors made of or protected by “materials resistant to corrosion by UF6”, and rotary shaft seals therefor;

 

 4. Equipment for fluorinating UF5 (solid) to UF6 (gas);

 

 5. Process systems for separating UF6 from carrier gas (e.g. nitrogen or argon) including:

 a. Cryogenic heat exchangers and cryoseparators capable of temperatures of 153 K (120°C) or less;

 b. Cryogenic refrigeration units capable of temperatures of 153 K (120°C) or less;

 c. UF6 cold traps capable of temperatures of 253 K (20°C) or less;

 

 6. “Lasers” or “laser” systems for the separation of uranium isotopes with a spectrum frequency stabiliser for operation over extended periods of time;

  N.B.:    SEE ALSO 6A005 AND 6A205.

 

 i. Equipment and components, specially designed or prepared for plasma separation process, as follows:

 

 1. Microwave power sources and antennae for producing or accelerating ions, with an output frequency greater than 30 GHz and mean power output greater than 50 kW;

 

 2. Radio frequency ion excitation coils for frequencies of more than 100 kHz and capable of handling more than 40 kW mean power;

 

 3. Uranium plasma generation systems;

 

 4. Liquid metal handling systems for molten uranium or uranium alloys, consisting of crucibles, made of or protected by suitable corrosion and heat resistant materials (e.g. tantalum, yttriacoated graphite, graphite coated with other rare earth oxides or mixtures thereof), and cooling equipment for the crucibles;

  N.B.:    SEE ALSO 2A225.

0B001 i. continued

 

 5. Product and tails collectors made of or protected by materials resistant to the heat and corrosion of uranium vapour such as yttriacoated graphite or tantalum;

 

 6. Separator module housings (cylindrical) for containing the uranium plasma source, radiofrequency drive coil and the product and tails collectors and made of a suitable nonmagnetic material (e.g. stainless steel);

 

 j. Equipment and components, specially designed or prepared for electromagnetic separation process, as follows:

 

 1. Ion sources, single or multiple, consisting of a vapour source, ioniser, and beam accelerator made of suitable nonmagnetic materials (e.g. graphite, stainless steel, or copper) and capable of providing a total ion beam current of 50 mA or greater;

 

 2. Ion collector plates for collection of enriched or depleted uranium ion beams, consisting of two or more slits and pockets and made of suitable nonmagnetic materials (e.g. graphite or stainless steel);

 

 3. Vacuum housings for uranium electromagnetic separators made of nonmagnetic materials (e.g. stainless steel) and designed to operate at pressures of 0.1 Pa or lower;

 

 4. Magnet pole pieces with a diameter greater than 2 m;

 

 5. High voltage power supplies for ion sources, having all of the following characteristics:

 a. Capable of continuous operation;

 b. Output voltage of 20,000 V or greater;

 c. Output current of 1 A or greater; and

 d. Voltage regulation of better than 0.01% over a period of 8 hours;

 N.B.:    SEE ALSO 3A227.

 

 6. Magnet power supplies (high power, direct current) having all of the following characteristics:

 a. Capable of continuous operation with a current output of 500 A or greater at a voltage of 100 V or greater; and

 b. Current or voltage regulation better than 0.01% over a period of 8 hours.

 N.B.:    SEE ALSO 3A226.

 

 

0B002 Specially designed or prepared auxiliary systems, equipment and components, as follows, for isotope separation plant specified in 0B001, made of or protected by “materials resistant to corrosion by UF6”:

 

 a. Feed autoclaves, ovens or systems used for passing UF6 to the enrichment process;

 

 b. Desublimers or cold traps, used to remove UF6 from the enrichment process for subsequent transfer upon heating;

 

 c. Product and tails stations for transferring UF6 into containers;

 

 d. Liquefaction or solidification stations used to remove UF6 from the enrichment process by compressing, cooling and converting UF6 to a liquid or solid form;

 

 e. Piping systems and header systems specially designed for handling UF6 within gaseous diffusion, centrifuge or aerodynamic cascades;

 

 f. 1. Vacuum manifolds or vacuum headers having a suction capacity of 5 m3/minute or more; or

  2. Vacuum pumps specially designed for use in UF6 bearing atmospheres;

 

 g. UF6 mass spectrometers/ion sources specially designed or prepared for taking online samples of feed, product or tails from UF6 gas streams and having all of the following characteristics:

 1. Unit resolution for mass of more than 320 amu;

 2. Ion sources constructed of or lined with nichrome or monel, or nickel plated;

 3. Electron bombardment ionisation sources; and

 4. Collector system suitable for isotopic analysis.

 

0B003 Plant for the conversion of uranium and equipment specially designed or prepared therefor, as follows:

 

 a. Systems for the conversion of uranium ore concentrates to UO3;

 b. Systems for the conversion of UO3 to UF6;

 c. Systems for the conversion of UO3 to UO2;

 d. Systems for the conversion of UO2 to UF4;

 e. Systems for the conversion of UF4 to UF6;

 f. Systems for the conversion of UF4 to uranium metal;

 g. Systems for the conversion of UF6 to UO2;

 h. Systems for the conversion of UF6 to UF4;

 i. Systems for the conversion of UO2 to UCl4.

 

 

0B004 Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows:

 

 a. Plant for the production of heavy water, deuterium or deuterium compounds, as follows:

 1. Waterhydrogen sulphide exchange plants;

 2. Ammoniahydrogen exchange plants;

 

 b. Equipment and components, as follows:

 

 1. Waterhydrogen sulphide exchange towers fabricated from fine carbon steel (e.g. ASTM A516) with diameters of 6 m to 9 m, capable of operating at pressures greater than or equal to 2 MPa and with a corrosion allowance of 6 mm or greater;

 

 2. Single stage, low head (i.e. 0.2 MPa) centrifugal blowers or compressors for hydrogen sulphide gas circulation (i.e. gas containing more than 70% H2S) with a throughput capacity greater than or equal to 56 m3/second when operating at pressures greater than or equal to 1.8 MPa suction and having seals designed for wet H2S service;

 

 3. Ammoniahydrogen exchange towers greater than or equal to 35 m in height with diameters of 1.5 m to 2.5 m capable of operating at pressures greater than 15 MPa;

 

 4. Tower internals, including stage contactors, and stage pumps, including those which are submersible, for heavy water production utilizing the ammoniahydrogen exchange process;

 

 5. Ammonia crackers with operating pressures greater than or equal to 3 MPa for heavy water production utilizing the ammoniahydrogen exchange process;

 

 6. Infrared absorption analysers capable of online hydrogen/deuterium ratio analysis where deuterium concentrations are equal to or greater than 90%;

 

 7. Catalytic burners for the conversion of enriched deuterium gas into heavy water utilizing the ammoniahydrogen exchange process;

 

 8. Complete heavy water upgrade systems, or columns therefor, for the upgrade of heavy water to reactorgrade deuterium concentration.

 

 

0B005 Plant specially designed for the fabrication of “nuclear reactor” fuel elements and specially designed or prepared equipment therefor.

 

 Note: A plant for the fabrication of “nuclear reactor” fuel elements includes equipment which:

  a. Normally comes into direct contact with or directly processes or controls the production flow of nuclear materials;

  b. Seals the nuclear materials within the cladding;

  c. Checks the integrity of the cladding or the seal; or

  d. Checks the finish treatment of the sealed fuel.

 

 

0B006 Plant for the reprocessing of irradiated “nuclear reactor” fuel elements, and specially designed or prepared equipment and components therefor.

 

 Note: 0B006 includes:

  a. Plant for the reprocessing of irradiated “nuclear reactor” fuel elements including equipment and components which normally come into direct contact with and directly control the irradiated fuel and the major nuclear material and fission product processing streams;

  b. Fuel element chopping or shredding machines, i.e. remotely operated equipment to cut, chop, shred or shear irradiated “nuclear reactor” fuel assemblies, bundles or rods;

  c. Dissolvers, critically safe tanks (e.g. small diameter, annular or slab tanks) specially designed or prepared for the dissolution of irradiated “nuclear reactor” fuel, which are capable of withstanding hot, highly corrosive liquids, and which can be remotely loaded and maintained;

  d. Countercurrent solvent extractors and ionexchange processing equipment specially designed or prepared for use in a plant for the reprocessing of irradiated “natural uranium”, “depleted uranium” or “special fissile materials”;

  e. Holding or storage vessels specially designed to be critically safe and resistant to the corrosive effects of nitric acid;

 Note: Holding or storage vessels may have the following features:

  1. Walls or internal structures with a boron equivalent (calculated for all constituent elements as defined in the note to 0C004) of at least two per cent;

  2. A maximum diameter of 175 mm for cylindrical vessels; or

  3. A maximum width of 75 mm for either a slab or annular vessel.

  f. Process control instrumentation specially designed or prepared for monitoring or controlling the reprocessing of irradiated “natural uranium”, “depleted uranium” or “special fissile materials”.

 

 

0B007 Plant for the conversion of plutonium and equipment specially designed or prepared therefor, as follows:

 

 a. Systems for the conversion of plutonium nitrate to oxide;

 b. Systems for plutonium metal production.

 

 

0C Materials

 

0C003 Deuterium, heavy water (deuterium oxide) and other compounds of deuterium, and mixtures and solutions containing deuterium, in which the isotopic ratio of deuterium to hydrogen exceeds 1:5,000.

 

 

0C004 Graphite, nuclear grade, having a purity level of less than 5 parts per million ‘boron equivalent’ and with a density greater than 1.5 g/cm3.

 N.B.: SEE ALSO 1C107

 

 Note 1: 0C004 does not control the following:

 

  a. Manufactures of graphite having a mass less than 1 kg, other than those specially designed or prepared for use in a nuclear reactor;

  b. Graphite powder.

 

 Note 2: In 0C004, ‘boron equivalent’ (BE) is defined as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:

 

  BEz (ppm) = CF x concentration of element Z in ppm;

 

  Z AB

 where CF is the conversion factor    = 

  B AZ

 

  and B  and Z  are the thermal neutron capture cross sections (in barns) for naturally occurring boron and element Z respectively; and AB and AZ are the atomic masses of naturally occurring boron and element Z respectively.

 

0C005 Specially prepared compounds or powders for the manufacture of gaseous diffusion barriers, resistant to corrosion by UF6 (e.g. nickel or alloy containing 60 weight per cent or more nickel, aluminium oxide and fully fluorinated hydrocarbon polymers), having a purity of 99.9 weight per cent or more and a mean particle size of less than 10 micrometres measured by American Society for Testing and Materials (ASTM) B330 standard and a high degree of particle size uniformity.

 

 

0D Software

 

0D001 “Software” specially designed or modified for the “development”, “production” or “use” of goods specified in this Category.

 

 

0E Technology

 

0E001 “Technology” according to the Nuclear Technology Note for the “development”, “production” or “use” of goods specified in this Category.

 

CATEGORY 1 MATERIALS, CHEMICALS, “MICROORGANISMS” & “TOXINS”

 

 

1A Systems, Equipment and Components

 

1A001 Components made from fluorinated compounds, as follows:

 

 a. Seals, gaskets, sealants or fuel bladders specially designed for “aircraft” or aerospace use made from more than 50 % by weight of any of the materials specified in 1C009.b. or 1C009.c.;

 

 b. Piezoelectric polymers and copolymers made from vinylidene fluoride materials specified in 1C009.a.:

 1. In sheet or film form; and

 2. With a thickness exceeding 200 µm;

 

 c. Seals, gaskets, valve seats, bladders or diaphragms made from fluoroelastomers containing at least one vinylether group as a constitutional unit, specially designed for “aircraft”, aerospace or ‘missile’ use.

 Note: In 1A001.c., ‘missile’ means complete rocket systems and unmanned aerial vehicle systems.

 

 

1A002 “Composite” structures or laminates, having any of the following:

 N.B: SEE ALSO 1A202, 9A010 and 9A110

 

 a. Consisting of an organic “matrix” and materials specified in 1C010.c., 1C010.d. or 1C010.e.; or

 

 b. Consisting of a metal or carbon “matrix”, and any of the following:

 1. Carbon “fibrous or filamentary materials” having all of the following:

 a. A “specific modulus” exceeding 10.15 x 106 m; and

 b. A “specific tensile strength” exceeding 17.7 x 104 m; or

 2. Materials specified in 1C010.c.

 

 Note 1: 1A002 does not control composite structures or laminates made from epoxy resin impregnated carbon “fibrous or filamentary materials” for the repair of “civil aircraft” structures or laminates, provided the size does not exceed 100 cm x 100 cm.

 Note 2: 1A002 does not control finished or semifinished items specially designed for purely civilian applications as follows:

  a. Sporting goods;

  b. Automotive industry;

  c. Machine tool industry;

  d. Medical applications.

 

 

1A003 Manufactures of nonfluorinated polymeric substances, specified in 1C008.a.3., in film, sheet, tape or ribbon form having any of the following:

 

 a. A thickness exceeding 0.254 mm; or

 

 b. Coated or laminated with carbon, graphite, metals or magnetic substances.

 

 Note: 1A003 does not control manufactures when coated or laminated with copper and designed for the production of electronic printed circuit boards.

 

 

1A004 Protective and detection equipment and components, other than those specified in military goods controls, as follows:

 N.B.: SEE ALSO 2B351 AND 2B352.

 

 a. Gas masks, filter canisters and decontamination equipment therefor, designed or modified for defence against any of the following, and specially designed components therefor:

 1. Biological agents “adapted for use in war”;

 2. Radioactive materials “adapted for use in war”;

 3. Chemical warfare (CW) agents; or

 4. “Riot control agents”, including:

 a. Bromobenzeneacetonitrile, (Bromobenzyl cyanide) (CA) (CAS 5798798);

 b. [(2chlorophenyl) methylene] propanedinitrile, (oChlorobenzylidenemalononitrile) (CS) (CAS 2698411);

 c. 2Chloro1phenylethanone, Phenylacyl chloride                         (chloroacetophenone) (CN) (CAS 532274);

 d. Dibenz(b,f)1,4oxazephine (CR) (CAS 257078);

 e. 10Chloro5,10dihydrophenarsazine, (Phenarsazine chloride), (Adamsite), (DM) (CAS 578949);

 f. NNonanoylmorpholine, (MPA) (CAS 5299649);

 

 b. Protective suits, gloves and shoes, specially designed or modified for defence against any of the following:

 1. Biological agents “adapted for use in war”;

 2. Radioactive materials “adapted for use in war”; or

 3. Chemical warfare (CW) agents;

 

 c. Nuclear, biological and chemical (NBC) detection systems, specially designed or modified for detection or identification of any of the following, and specially designed components therefor:

 1. Biological agents “adapted for use in war”;

 2. Radioactive materials “adapted for use in war”; or

 3. Chemical warfare (CW) agents.

1A004 continued

 

 Note: 1A004 does not control:

  a. Personal radiation monitoring dosimeters;

  b.  Equipment limited by design or function to protect against hazards specific to civil industries, such as mining, quarrying, agriculture, pharmaceuticals, medical, veterinary, environmental, waste management, or to the food industry.

 

 Technical Notes:

1. 1A004 includes equipment and components that have been identified, successfully tested to national standards or otherwise proven effective, for the detection of or defence against radioactive materials “adapted for use in war”, biological agents “adapted for use in war”, chemical warfare agents, ‘simulants’ or “riot control agents”, even if such equipment or components are used in civil industries such as mining, quarrying, agriculture, pharmaceuticals, medical, veterinary, environmental, waste management, or the food industry.

2. ‘Simulant’ is a substance or material that is used in place of toxic agent (chemical or biological) in training, research, testing or evaluation.

 

 

1A005 Body armour, and specially designed components therefor, other than those manufactured to military standards or specifications or to their equivalents in performance.

 N.B.: SEE ALSO ML13.

 

 N.B.: For “fibrous or filamentary materials” used in the manufacture of body armour, see 1C010.

 

 Note 1: 1A005 does not control body armour or protective garments when accompanying their user for the user’s own personal protection.

 Note 2: 1A005 does not control body armour designed to provide frontal protection only from both fragment and blast from nonmilitary explosive devices.

 

 

1A006 Equipment, specially designed or modified for the disposal of improvised explosive devices, as follows, and specially designed components and accessories therefor:

 N.B.: SEE ALSO ML4.b.

 

 a. Remotely operated vehicles;

 b. Disruptors’.

 Technical Note:

 Disruptors’ are devices specially designed for the purpose of preventing the operation of an explosive device by projecting a liquid, solid or frangible projectile.

 

 Note: 1A006 does not control equipment when accompanying its operator.

1A007 Equipment and devices, specially designed to initiate charges and devices containing               energetic materials, by electrical means, as follows:

 N.B.: SEE ALSO ML4.a., ML4.b., ML909, 3A229 AND 3A232.

 

 a. Explosive detonator firing sets designed to drive explosive detonators specified in 1A007.b.;

 

 b. Electrically driven explosive detonators as follows:

1. Exploding bridge (EB);

2. Exploding bridge wire (EBW);

3. Slapper;

4. Exploding foil initiators (EFI).

 

 Technical Notes:

1. The word initiator or igniter is sometimes used in place of the word detonator.

2. For the purpose of 1A007.b. the detonators of concern all utilise a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporises when a fast, highcurrent electrical pulse is passed through it. In non slapper types, the exploding conductor starts a chemical detonation in a contacting high explosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slappertype detonator.

 

 

1A102 Resaturated pyrolized carboncarbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

1A202 Composite structures, not controlled in 1A002, in the form of tubes and having both of the following characteristics:

 N.B.: SEE ALSO 9A010 AND 9A110.

 

 a. An inside diameter of between 75 mm and 400 mm; and

 b. Made with any of the “fibrous or filamentary materials” specified in 1C010.a. or b. or 1C210.a. or with carbon prepreg materials specified in 1C210.c.

 

 

1A225 Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.

 

1A226 Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:

 

 a. Made of phosphor bronze mesh chemically treated to improve wettability; and

 b. Designed to be used in vacuum distillation towers.

 

 

1A227 Highdensity (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:

 

 a. A ‘cold area’ greater than 0.09 m2;

 b. A density greater than 3 g/cm3; and

 c. A thickness of 100 mm or greater.

 

 Technical Note:

 In 1A227 the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application.

 

 

1B Test, Inspection and Production Equipment

 

1B001 Equipment for the production of fibres, prepregs, preforms or “composites”, specified in 1A002 or 1C010, as follows, and specially designed components and accessories therefor:

 N.B.: SEE ALSO 1B101 AND 1B201.

 

 a. Filament winding machines of which the motions for positioning, wrapping and winding fibres are coordinated and programmed in three or more axes, specially designed for the manufacture of “composite” structures or laminates from “fibrous or filamentary materials”;

 

 b. Tapelaying or towplacement machines of which the motions for positioning and laying tape, tows or sheets are coordinated and programmed in two or more axes, specially designed for the manufacture of “composite” airframe or ‘missile’ structures;

 Note: In 1B001.b., ‘missile’ means complete rocket systems and unmanned aerial vehicle systems.

 

 c. Multidirectional, multidimensional weaving machines or interlacing machines, including adapters and modification kits, for weaving, interlacing or braiding fibres to manufacture “composite” structures;

 Technical Note:

 For the purposes of 1B001.c., the technique of interlacing includes knitting.

 

 Note: 1B001.c. does not control textile machinery not modified for the above enduses.

 

1B001 continued

 

 d. Equipment specially designed or adapted for the production of reinforcement fibres, as follows:

 

 1. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, pitch or polycarbosilane) into carbon fibres or silicon carbide fibres, including special equipment to strain the fibre during heating;

 

 2. Equipment for the chemical vapour deposition of elements or compounds on heated filamentary substrates to manufacture silicon carbide fibres;

 

 3. Equipment for the wetspinning of refractory ceramics (such as aluminium oxide);

 

 4. Equipment for converting aluminium containing precursor fibres into alumina fibres by heat treatment;

 

 e. Equipment for producing prepregs specified in 1C010.e. by the hot melt method;

 

 f. Nondestructive inspection equipment specially designed for “composite” materials, as follows:

 

1. Xray tomography systems for three dimensional defect inspection;

 

2. Numerically controlled ultrasonic testing machines of which the motions for positioning transmitters and/or receivers are simultaneously coordinated and programmed in four or more axes to follow the three dimensional contours of the component under inspection.

 

 

1B002 Equipment for producing metal alloys, metal alloy powder or alloyed materials,

 specially designed to avoid contamination and specially designed for use in one

 of the processes specified in 1C002.c.2.

 N.B.: SEE ALSO 1B102.

 

 

1B003 Tools, dies, moulds or fixtures, for “superplastic forming” or “diffusion bonding”

 titanium, aluminium or their alloys, specially designed for the manufacture of any of the following:

 a. Airframe or aerospace structures;

 b. “Aircraft” or aerospace engines; or

 c. Specially designed components for those structures or engines.

 

 

1B101 Equipment, other than that specified in 1B001, for the “production” of structural composites as follows; and specially designed components and accessories therefor:

 N.B.: SEE ALSO 1B201.

 

 Note: Components and accessories specified in 1B101 include moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof.

 

 a. Filament winding machines of which the motions for positioning, wrapping

  and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and coordinating and programming controls;

 

 b. Tapelaying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes, designed for the manufacture of composite airframe and “missile” structures;

 

 c. Equipment designed or modified for the “production” of “fibrous or filamentary materials” as follows:

 

 1. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon or polycarbosilane) including special provision to strain the fibre during heating;

 

 2. Equipment for the vapour deposition of elements or compounds on heated filament substrates;

 

 3. Equipment for the wetspinning of refractory ceramics (such as aluminium oxide);

 

 d. Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry 9C110.

 Note: 1B101.d. includes rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.

 

 

1B102 Metal powder “production equipment”, other than that specified in 1B002, and

 components as follows:

 N.B.: SEE ALSO 1B115.b.

 

 a. Metal powder “production equipment” usable for the “production”, in a controlled environment, of spherical or atomised materials specified in 1C011.a., 1C011.b., 1C111.a.1., 1C111.a.2. or in ML8.a.

 

 b. Specially designed components for “production equipment” specified in 1B002 or 1B102.a.

 

1B102 continued

 

 Note: 1B102 includes:

  a. Plasma generators (high frequency arcjet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argonwater environment;

  b. Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argonwater environment;

  c. Equipment usable for the “production” of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).

 

 

1B115 Equipment, other than that specified in 1B002 or 1B102, for the production of propellant and propellant constituents, as follows, and specially designed components therefor:

 

 a. “Production equipment” for the “production”, handling or acceptance testing of liquid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in ML8;

 

 b. “Production equipment” for the “production”, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in ML8.

 Note: 1B115.b. does not control batch mixers, continuous mixers or fluid energy mills.  For the control of batch mixers, continuous mixers and fluid energy mills see 1B117, 1B118 and 1B119.

 

 Note 1: For equipment specially designed for the production of military goods, see the Munitions List.

 Note 2: 1B115 does not control equipment for the “production”, handling and acceptance testing of boron carbide.

 

 

1B116 Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1,573 K (1,300oC) to 3,173 K (2,900oC) temperature range at pressures of 130 Pa to 20 kPa.

 

 

1B117 Batch mixers with provision for mixing under vacuum in the range of zero to 13.326 kPa and with temperature control capability of the mixing chamber and having all of the following, and specially designed components therefor:

 

 a. A total volumetric capacity of 110 litres or more; and

 

 b. At least one mixing/kneading shaft mounted off centre.

 

 

1B118 Continuous mixers with provision for mixing under vacuum in the range of zero to 13.326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor:

 

 a. Two or more mixing/kneading shafts; or

 

 b. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber.

 

 

1B119 Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Munitions List, and specially designed components therefor.

 

 

1B201 Filament winding machines, not controlled in 1B001 or 1B101, and related equipment, as follows:

 

 a. Filament winding machines having all of the following characteristics:

 1. Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes;

 2. Specially designed to fabricate composite structures or laminates from “fibrous or filamentary materials”; and

 3. Capable of winding cylindrical rotors of diameter between 75 and 400 mm and lengths of 600 mm or greater;

 

 b. Coordinating and programming controls for the filament winding machines specified in 1B201.a.;

 

 c. Precision mandrels for the filament winding machines specified in 1B201.a.

 

 

1B225 Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.

 

 

1B226 Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.

 

 Note: 1B226 includes separators:

  a. Capable of enriching stable isotopes;

  b. With the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.

 

 

1B227 Ammonia synthesis converters or ammonia synthesis units, in which the synthesis gas (nitrogen and hydrogen) is withdrawn from an ammonia/hydrogen highpressure exchange column and the synthesized ammonia is returned to said column.

 

 

1B228 Hydrogencryogenic distillation columns having all of the following characteristics:

 

 a. Designed for operation with internal temperatures of 35 K (238°C) or less;

 b. Designed for operation at an internal pressure of 0.5 to 5 MPa;

 c. Constructed of either:

 1. Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or

 2. Equivalent materials which are both cryogenic and H2compatible; and

 d. With internal diameters of 1 m or greater and effective lengths of 5 m or greater.

 

 

1B229 Waterhydrogen sulphide exchange tray columns and ‘internal contactors’, as follows:

 

 N.B.: For columns which are specially designed or prepared for the production of heavy water see 0B004.

 

 a. Waterhydrogen sulphide exchange tray columns, having all of the following characteristics:

 1. Can operate at pressures of 2 MPa or greater;

 2. Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and

 3. With a diameter of 1.8 m or greater;

 

 b. ‘Internal contactors’ for the waterhydrogen sulphide exchange tray columns specified in 1B229.a.

 Technical Note:

 ‘Internal contactors’ of the columns are segmented trays which have an effective assembled diameter of 1.8 m or greater, are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0.03% or less.  These may be sieve trays, valve trays, bubble cap trays, or turbogrid trays.

 

 

1B230 Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:

 

 a. Airtight (i.e., hermetically sealed);

 b. A capacity greater than 8.5 m3/h; and

 c. Either of the following characteristics:

 1. For concentrated potassium amide solutions (1% or greater), an operating pressure of 1.5 to 60 MPa; or

 2. For dilute potassium amide solutions (less than 1%), an operating pressure of 20 to 60 MPa.

 

 

1B231 Tritium facilities or plants, and equipment therefor, as follows:

 

 a. Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;

 

 b. Equipment for tritium facilities or plants, as follows:

 1. Hydrogen or helium refrigeration units capable of cooling to 23 K (250°C) or less, with heat removal capacity greater than 150 W;

 2. Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.

 

 

1B232 Turboexpanders or turboexpandercompressor sets having both of the following characteristics:

 

 a. Designed for operation with an outlet temperature of 35 K (238°C) or less; and

 

 b. Designed for a throughput of hydrogen gas of 1000 kg/h or greater.

 

 

1B233 Lithium isotope separation facilities or plants, and equipment therefor, as follows:

 

 a. Facilities or plants for the separation of lithium isotopes;

 

 b. Equipment for the separation of lithium isotopes, as follows:

 1. Packed liquidliquid exchange columns specially designed for lithium amalgams;

 2. Mercury or lithium amalgam pumps;

 3. Lithium amalgam electrolysis cells;

 4. Evaporators for concentrated lithium hydroxide solution.

 

 

1C Materials

 

 Technical Note:

 

 Metals and alloys:

 Unless provision to the contrary is made, the words ‘metals’ and ‘alloys’ in 1C001 to 1C012 cover crude and semifabricated forms, as follows:

 

 Crude forms:

 Anodes, balls, bars (including notched bars and wire bars), billets, blocks, blooms, brickets, cakes, cathodes, crystals, cubes, dice, grains, granules, ingots, lumps, pellets, pigs, powder, rondelles, shot, slabs, slugs, sponge, sticks;

 

1C Materials continued

 

 Semifabricated forms (whether or not coated, plated, drilled or punched):

 a. Wrought or worked materials fabricated by rolling, drawing, extruding, forging, impact extruding, pressing, graining, atomising, and grinding, i.e.: angles, channels, circles, discs, dust, flakes, foils and leaf, forging, plate, powder, pressings and stampings, ribbons, rings, rods (including bare welding rods, wire rods, and rolled wire), sections, shapes, sheets, strip, pipe and tubes (including tube rounds, squares, and hollows), drawn or extruded wire;

 b. Cast material produced by casting in sand, die, metal, plaster or other types of moulds, including high pressure castings, sintered forms, and forms made by powder metallurgy.

 

 The object of the control should not be defeated by the export of nonlisted forms alleged to be finished products but representing in reality crude forms or semifabricated forms.

 

 

1C001 Materials specially designed for use as absorbers of electromagnetic waves, or

 intrinsically conductive polymers, as follows:

 N.B.: SEE ALSO 1C101.

 

 a. Materials for absorbing frequencies exceeding 2 x 108 Hz but less than 3 x 1012 Hz;

 Note 1: 1C001.a. does not control:

  a. Hair type absorbers, constructed of natural or synthetic fibres, with nonmagnetic loading to provide absorption;

  b. Absorbers having no magnetic loss and whose incident surface is nonplanar in shape, including pyramids, cones, wedges and convoluted surfaces;

  c. Planar absorbers, having all of the following:

   1. Made from any of the following:

    a. Plastic foam materials (flexible or nonflexible) with carbonloading, or organic materials, including binders, providing more than 5% echo compared with metal over a bandwidth exceeding ±15% of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 450 K (177°C); or

    b. Ceramic materials providing more than 20% echo compared with metal over a bandwidth exceeding ±15% of the centre frequency of the incident energy, and not capable of withstanding temperatures exceeding 800 K (527°C);

1C001 a. continued

 

 Technical Note:

 Absorption test samples for 1C001.a. Note: 1.c.1. should be a square at least 5 wavelengths of the centre frequency on a side and positioned in the far field of the radiating element.

   2. Tensile strength less than 7 x 106 N/m2; and

   3. Compressive strength less than 14 x 106 N/m2;

  d. Planar absorbers made of sintered ferrite, having all of the following:

   1. A specific gravity exceeding 4.4; and

   2. A maximum operating temperature of 548 K (275°C).

 Note 2: Nothing in Note 1 to 1C001.a. releases magnetic materials to provide absorption when contained in paint.

 

 b. Materials for absorbing frequencies exceeding 1.5 x 1014 Hz but less than 3.7 x 1014 Hz and not transparent to visible light;

 

 c. Intrinsically conductive polymeric materials with a ‘bulk electrical conductivity’ exceeding 10,000 S/m (Siemens per metre) or a ‘sheet (surface) resistivity’ of less than 100 ohms/square, based on any of the following polymers:

 1. Polyaniline;

 2. Polypyrrole;

 3. Polythiophene;

 4. Poly phenylenevinylene; or

 5. Poly thienylenevinylene.

 Technical Note:

 ‘Bulk electrical conductivity’ and ‘sheet (surface) resistivity’ should be determined using ASTM D257 or national equivalents.

 

 

1C002 Metal alloys, metal alloy powder and alloyed materials, as follows:

 N.B.: SEE ALSO 1C202.

 

 Note: 1C002 does not control metal alloys, metal alloy powder and alloyed materials for coating substrates.

 

 Technical Notes:

 1. The metal alloys in 1C002 are those containing a higher percentage by weight of the stated metal than of any other element.

 2. ‘Stressrupture life’ should be measured in accordance with ASTM standard E139 or national equivalents.

 

1C002 continued

 

 3. ‘Low cycle fatigue life’ should be measured in accordance with ASTM Standard E606 ‘Recommended Practice for ConstantAmplitude LowCycle Fatigue Testing’ or national equivalents. Testing should be axial with an average stress ratio equal to 1 and a stressconcentration factor (Kt) equal to 1. The average stress is defined as maximum stress minus minimum stress divided by maximum stress.

 

 a. Aluminides, as follows:

 

 1. Nickel aluminides containing a minimum of 15 % by weight aluminium, a maximum of 38 % by weight aluminium and at least one additional alloying element;

 

 2. Titanium aluminides containing 10 % by weight or more aluminium and at least one additional alloying element;

 

 b. Metal alloys, as follows, made from material specified in 1C002.c.:

 

 1. Nickel alloys having any of the following:

  1. A ‘stressrupture life’ of 10,000 hours or longer at 923 K (650°C) at a stress of 676 MPa; or

 b. A ‘low cycle fatigue life’ of 10,000 cycles or more at 823 K (550° C) at a maximum stress of 1,095 MPa;

 

 2. Niobium alloys having any of the following:

 a. A ‘stressrupture life’ of 10,000 hours or longer at 1,073 K (800°C) at a stress of 400 MPa; or

 b. A ‘low cycle fatigue life’ of 10,000 cycles or more at 973 K (700°C) at a maximum stress of 700 MPa;

 

 3. Titanium alloys having any of the following:

 a. A ‘stressrupture life’ of 10,000 hours or longer at 723 K (450°C) at a stress of 200 MPa; or

 b. A ‘low cycle fatigue life’ of 10,000 cycles or more at 723 K (450°C) at a maximum stress of 400 MPa;

 

 4. Aluminium alloys having any of the following:

 a. A tensile strength of 240 MPa or more at 473 K (200°C); or

 b. A tensile strength of 415 MPa or more at 298 K (25°C);

 

 5. Magnesium alloys having any of the following:

 a. A tensile strength of 345 MPa or more; and

 b. A corrosion rate of less than 1 mm/year in 3% sodium chloride aqueous solution measured in accordance with ASTM standard G31 or national equivalents;

 

 

1C002 continued

 

 c. Metal alloy powder or particulate material for material, having all of the following:

 

 1. Made from any of the following composition systems:

 

 Technical Note:

 X in the following equals one or more alloying elements.

 

 a. Nickel alloys (NiAlX, NiXAl) qualified for turbine engine parts or components, i.e. with less than 3 nonmetallic particles (introduced during the manufacturing process) larger than 100 µm in 109 alloy particles;

 

 b. Niobium alloys (NbAlX or NbXAl, NbSiX or NbXSi, NbTiX or NbXTi);

 

 c. Titanium alloys (TiAlX or TiXAl);

 

 d. Aluminium alloys (AlMgX or AlXMg, AlZnX or AlXZn, AlFeX or AlXFe); or

 

 e. Magnesium alloys (MgAlX or MgXAl);

 

 2. Made in a controlled environment by any of the following processes:

 a. “Vacuum atomisation”;

 b. “Gas atomisation”;

 c. “Rotary atomisation”;

 d. “Splat quenching”;

 e. “Melt spinning” and “comminution”;

 f. “Melt extraction” and “comminution”; or

 g. “Mechanical alloying”; and

 

 3. Capable of forming materials specified in 1C002.a. or 1C002.b.

 

 d. Alloyed materials having all of the following:

 

 1. Made from any of the composition systems specified in 1C002.c.1.;

 

 2. In the form of uncomminuted flakes, ribbons or thin rods; and

 

 3. Produced in a controlled environment by any of the following:

 a. “Splat quenching”;

 b. “Melt spinning”; or

 c.  “Melt extraction”.

 


 

1C003 Magnetic metals, of all types and of whatever form, having any of the following:             

 a. Initial relative permeability of 120,000 or more and a thickness of 0.05 mm or less;

 Technical Note:

 Measurement of initial permeability must be performed on fully annealed materials.

 

 b. Magnetostrictive alloys, having any of the following:

 1. A saturation magnetostriction of more than 5 x 104; or

 2. A magnetomechanical coupling factor (k) of more than 0.8; or

 

 c. Amorphous or ‘nanocrystalline’ alloy strips, having all of the following characteristics:

 1. A composition having a minimum of 75 % by weight of iron, cobalt or nickel;

 2. A saturation magnetic induction (Bs) of 1.6 T or more; and

 3. Any of the following:

 a. A strip thickness of 0.02 mm or less; or

 b. An electrical resistivity of 2 x 104 ohm cm or more.

 Technical Note:

 ‘Nanocrystalline’ materials in 1C003.c. are those materials having a crystal grain size of 50 nm or less, as determined by Xray diffraction.

 

 

1C004 Uranium titanium alloys or tungsten alloys with a “matrix” based on iron, nickel or copper, having all of the following:

 

 a. A density exceeding 17.5 g/cm3;

 b. An elastic limit exceeding 880 MPa;

 c. An ultimate tensile strength exceeding 1,270 MPa; and

 d. An elongation exceeding 8%.

 

 

1C005 “Superconductive” “composite” conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows:

 

 a. “Superconductive” “composite” conductors containing one or more niobiumtitanium filaments, having all of the following:

 1. Embedded in a “matrix” other than a copper or copperbased mixed “matrix”; and

 2. Having a crosssection area less than 0.28 x 104 mm2 (6 µm in diameter for circular filaments);

 

 b. “Superconductive” “composite” conductors consisting of one or more “superconductive” filaments other than niobiumtitanium, having all of the following:

 

1C005 b. continued

 

 1. A “critical temperature” at zero magnetic induction exceeding 9.85 K (263.31°C); and

 2. Remaining in the “superconductive” state at a temperature of 4.2 K

  (268.96°C) when exposed to a magnetic field oriented in any direction perpendicular to the longitudinal axis of conductor and corresponding to a magnetic induction of 12 T with critical current density exceeding 1,750 A/mm2 on overall crosssection of the conductor;

 

 c. “Superconductive” “composite” conductors consisting of one or more “superconductive” filaments which remain “superconductive” above 115 K (158.16°C).

 

 Technical Note:

For the purpose of 1C005 filaments may be in wire, cylinder, film, tape or ribbon form.

 

 

1C006 Fluids and lubricating materials, as follows:

 

 a. Hydraulic fluids containing, as their principal ingredients, any of the following compounds or materials:

 

 1. Synthetic ‘silahydrocarbon oils’, having all of the following:

 Technical Note:

 For the purpose of 1C006.a.1., ‘silahydrocarbon oils’ contain exclusively silicon, hydrogen and carbon.

 a. A ‘flash point’ exceeding 477 K (204°C);

 b. A ‘pour point’ at 239 K (34°C) or less;

 c. A ‘viscosity index’ of 75 or more; and

 d. A ‘thermal stability’ at 616 K (343°C); or

 

 2. ‘Chlorofluorocarbons’, having all of the following:

 Technical Note:

 For the purpose of 1C006.a.2., ‘chlorofluorocarbons’ contain exclusively carbon, fluorine and chlorine.

 a. No ‘flash point’;

 b. An ‘autogenous ignition temperature’ exceeding 977 K (704°C);

 c. A ‘pour point’ at 219 K (54°C) or less;

 d. A ‘viscosity index’ of 80 or more; and

 e. A boiling point at 473 K (200°C) or higher;

 

 b. Lubricating materials containing, as their principal ingredients, any of the following:

 

 1. Phenylene or alkylphenylene ethers or thioethers, or their mixtures, containing more than two ether or thioether functions or mixtures thereof; or

 

 

1C006 b. continued

 

 2. Fluorinated silicone fluids with a kinematic viscosity of less than 5,000 mm2/s (5,000 centistokes) measured at 298 K (25°C);

 

 c. Damping or flotation fluids with a purity exceeding 99.8%, containing less than 25 particles of 200 µm or larger in size per 100 ml and made from at least 85% of any of the following compounds or materials:

 

 1. Dibromotetrafluoroethane;

 2. Polychlorotrifluoroethylene (oily and waxy modifications only); or

 3. Polybromotrifluoroethylene;

 

 d. Fluorocarbon electronic cooling fluids having all of the following:

 1. Containing 85% by weight or more of any of the following, or mixtures thereof:

 a. Monomeric forms of perfluoropolyalkylethertriazines or perfluoroaliphaticethers;

 b. Perfluoroalkylamines;

 c. Perfluorocycloalkanes; or

 d. Perfluoroalkanes;

 2. Density at 298 K (25°C) of 1.5 g/ml or more;

 3. In a liquid state at 273 K (0°C); and

 4. Containing 60% or more by weight of fluorine.

 

 Technical Note:

 For the purpose of 1C006:

 1. ‘Flash point’ is determined using the Cleveland Open Cup Method described in ASTM D92 or national equivalents;

 2. ‘Pour point’ is determined using the method described in ASTM D97 or national equivalents;

 3. ‘Viscosity index’ is determined using the method described in ASTM D2270 or national equivalents;

 4. ‘Thermal stability’ is determined by the following test procedure or national equivalents:

  Twenty ml of the fluid under test is placed in a 46 ml type 317 stainless steel chamber containing one each of 12.5 mm (nominal) diameter balls of M10 tool steel, 52100 steel and naval bronze (60% Cu, 39% Zn, 0.75% Sn);

  The chamber is purged with nitrogen, sealed at atmospheric pressure and the temperature raised to and maintained at 644 ± 6 K (371 ± 6°C) for six hours;

  The specimen will be considered thermally stable if, on completion of the above procedure, all of the following conditions are met:

 a. The loss in weight of each ball is less than 10 mg/mm2 of ball surface;

 b. The change in original viscosity as determined at 311 K (38°C) is less than 25%; and

 c. The total acid or base number is less than 0.40;

 5. ‘Autogenous ignition’ temperature is determined using the method described in ASTM E659 or national equivalents.

 

 

1C007 Ceramic base materials, non“composite” ceramic materials, ceramic“matrix”

 “composite” materials and precursor materials, as follows:

 N.B.: SEE ALSO 1C107.

 

 a. Base materials of single or complex borides of titanium having total metallic impurities, excluding intentional additions, of less than 5,000 ppm, an average particle size equal to or less than 5 µm and no more than 10% of the particles larger than 10 µm;

 

 b. Non“composite” ceramic materials in crude or semifabricated form, composed of borides of titanium with a density of 98% or more of the theoretical density;

 Note: 1C007.b. does not control abrasives.

 

 c. Ceramicceramic “composite” materials with a glass or oxide“matrix” and reinforced with fibres having all of the following:

 1. Made from any of the following materials:

 a. SiN;

 b. SiC;

 c. SiAlON; or

 d. SiON; and

 2. Having a “specific tensile strength” exceeding 12.7 x 103m;

 

 d. Ceramicceramic “composite” materials, with or without a continuous metallic phase, incorporating particles, whiskers or fibres, where carbides or nitrides of silicon, zirconium or boron form the “matrix”;

 

 e. Precursor materials (i.e., special purpose polymeric or metalloorganic materials) for producing any phase or phases of the materials specified in 1C007.c., as follows:

 1. Polydiorganosilanes (for producing silicon carbide);

 2. Polysilazanes (for producing silicon nitride);

 3. Polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components);

 

 f. Ceramicceramic “composite” materials with an oxide or glass “matrix” reinforced with continuous fibres from any of the following systems:

 1. Al2O3; or

 2. SiCN.

 Note: 1C007.f. does not control “composites” containing fibres from these systems with a fibre tensile strength of less than 700 MPa at 1,273 K (1,000°C) or fibre tensile creep resistance of more than 1% creep strain at 100 MPa load and 1,273 K (1,000°C) for 100 hours.


1C008 Nonfluorinated polymeric substances as follows:

 

 a. 1. Bismaleimides;

 2. Aromatic polyamideimides;

 3. Aromatic polyimides;

 4. Aromatic polyetherimides having a glass transition temperature (Tg) exceeding 513 K (240°C);

 Note 1: 1C008.a. controls the substances in liquid or solid form, including resin, powder, pellet, film, sheet, tape or ribbon;

 

 Note 2: 1C008.a. does not control nonfusible compression moulding powders or moulded forms.

 

 b. Thermoplastic liquid crystal copolymers having a heat distortion temperature exceeding 523 K (250°C) measured according to ISO 752 (2004), method A or national equivalents, with a load of 1.80 N/mm2 and composed of:

 1. Any of the following:

 a. Phenylene, biphenylene or naphthalene; or

 b. Methyl, tertiarybutyl or phenyl substituted phenylene, biphenylene or naphthalene; and

 2. Any of the following:

 a. Terephthalic acid;

 b. 6hydroxy2 naphthoic acid; or

 c. 4hydroxybenzoic acid;

 

 c. Deleted;

 

 d. Polyarylene ketones;

 

 e. Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof;

 

 f. Polybiphenylenethersulphone having a ‘glass transition temperature (Tg) ‘ exceeding 513 K (240°C).

 

 Technical Note:

 The ‘glass transition temperature (Tg)’ for 1C008 materials is determined using the method described in ISO 113572 (1999) or national equivalents.

 

1C009 Unprocessed fluorinated compounds as follows:

 

 a. Copolymers of vinylidene fluoride having 75% or more beta crystalline structure without stretching;

 

 b. Fluorinated polyimides containing 10% by weight or more of combined fluorine;

 

 c. Fluorinated phosphazene elastomers containing 30% by weight or more of combined fluorine.

 

1C010 “Fibrous or filamentary materials”, which may be used in organic “matrix”, metallic “matrix” or carbon “matrix” “composite” structures or laminates, as follows:

 N.B.: SEE ALSO 1C210.

 

 a. Organic “fibrous or filamentary materials”, having all of the following:

 1. A “specific modulus” exceeding 12.7 x 106 m; and

 2. A “specific tensile strength” exceeding 23.5  x 104 m;

 Note: 1C010.a. does not control polyethylene.

 

 b. Carbon “fibrous or filamentary materials”, having all of the following:

 1. A “specific modulus” exceeding 12.7 x 106 m; and

 2. A “specific tensile strength” exceeding 23.5 x 104 m;

 Note: 1C010.b. does not control fabric made from “fibrous or filamentary materials” for the repair of “civil aircraft” structures or laminates, in which the size of individual sheets does not exceed 100 cm x 100 cm.

 Technical Note:

 Properties for materials described in 1C010.b. should be determined using SACMA recommended methods SRM 12 to 17, or national equivalent tow tests, such as Japanese Industrial Standard JISR7601, Paragraph 6.6.2., and based on lot average.

 

 c. Inorganic “fibrous or filamentary materials”, having all of the following:

 1. A “specific modulus” exceeding 2.54 x 106 m; and

 2. A melting, softening, decomposition or sublimation point exceeding 1,922 K (1,649°C) in an inert environment;

 Note: 1C010.c. does not control:

  a. Discontinuous, multiphase, polycrystalline alumina fibres in chopped fibre or random mat form, containing 3 % by weight or more silica, with a “specific modulus” of less than 10 x 106 m;

  b. Molybdenum and molybdenum alloy fibres;

  c. Boron fibres;

  d. Discontinuous ceramic fibres with a melting, softening, decomposition or sublimation point lower than 2,043 K (1,770°C) in an inert environment.

 

 d. “Fibrous or filamentary materials”, having any of the following:

 1. Composed of any of the following:

 a. Polyetherimides specified in 1C008.a.; or

 b. Materials specified in 1C008.b. to 1C008.f.; or

 2. Composed of materials specified in 1C010.d.1.a. or 1C010.d.1.b. and “commingled” with other fibres specified in 1C010.a., 1C010.b. or 1C010.c.;

 

1C010 continued

 

 e. Resinimpregnated or pitchimpregnated fibres (prepregs), metal or carboncoated fibres (preforms) or “carbon fibre preforms”, as follows:

 

 1. Made from “fibrous or filamentary materials” specified in 1C010.a., 1C010.b. or 1C010.c.;

 

 2. Made from organic or carbon “fibrous or filamentary materials”, having any of the following:

 a. A “specific tensile strength” exceeding 17.7 x 104 m;

 b. A “specific modulus” exceeding 10.15 x 106 m;

 c. Not specified in 1C010.a. or 1C010.b.; and

 d. When impregnated with materials specified in 1C008 or 1C009.b., having a glass transition temperature (Tg) exceeding 383 K (110°C) or with phenolic or epoxy resins, having a glass transition temperature (Tg) equal to or exceeding 418 K (145°C).

 

 Notes: 1C010.e. does not control:

  a. Epoxy resin “matrix” impregnated carbon “fibrous or filamentary materials” (prepregs) for the repair of “civil aircraft” structures or laminates, in which the size of individual sheets of prepreg does not exceed 100 cm x 100 cm;

  b. Prepregs when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160°C) and a cure temperature lower than the glass transition temperature (Tg).

 

 Technical Note:

 The glass transition temperature (Tg) for 1C010.e. materials is  determined using the method described in ASTM D 3418 using the dry method.  The glass transition temperature (Tg) for phenolic and epoxy resins is determined using the method described in ASTM D 4065 at a frequency of 1Hz and a heating rate of 2 K (°C) per minute using the dry method.

 

 

1C011 Metals and compounds, as follows:

 N.B.: SEE ALSO ML8.a.1., ML8.a.2. AND 1C111.

 

 a. Metals in particle sizes of less than 60 µm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99% or more of zirconium, magnesium and alloys thereof;

 Technical Note:

 The natural content of hafnium in the zirconium (typically 2% to 7%) is counted with the zirconium.

 Note: The metals or alloys specified in 1C011.a. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.

1C011 continued

 

 b. Boron or boron carbide of 85% purity or higher, and a particle size of 60 µm or less;

 Note: The metals or alloys specified in 1C011.b. are controlled whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.

 

 c. Guanidine nitrate;

 

 d. Nitroguanidine (NQ) (CAS 556887).

 

 

1C012 Materials as follows:

 Technical Note:

 These materials are typically used for nuclear heat sources.

 

 a. Plutonium in any form with a plutonium isotopic assay of plutonium238 of more than 50% by weight;

 Note: 1C012.a. does not control:

  a. Shipments with a plutonium content of 1 g or less;

  b. Shipments of 3 “effective grams” or less when contained in a sensing component in instruments.

 

 b. “Previously separated” neptunium237 in any form.

 Note: 1C012.b. does not control shipments with a neptunium237 content of 1 g or less.

 

 

1C101 Materials and devices for reduced observables such as radar reflectivity,

 ultraviolet/infrared signatures and acoustic signatures, not controlled

 in 1C001, usable in ‘missiles’, “missile” subsystems or unmanned aerial vehicles specified in 9A012.

 Note 1: 1C101 includes:

  a. Structural materials and coatings specially designed for reduced radar reflectivity;

  b. Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultraviolet regions of the electromagnetic spectrum.

 Note 2: 1C101 does not include coatings when specially used for the thermal control of satellites.

 

Technical Note:

In 1C101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

1C102 Resaturated pyrolized carboncarbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

1C107 Graphite and ceramic materials, not controlled in 1C007, as follows:

 

 a. Fine grain graphites with a bulk density of 1.72 g/cm3 or greater, measured at 288 K (15°C), and having a grain size of 100 µm or less, usable for rocket nozzles and reentry vehicle nose tips, which can be machined to any of the following products:

 1. Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;

 2. Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or

 3. Blocks having a size of 120 mm x 120 mm x 50 mm or greater;

 N.B.: SEE ALSO 0C004

 b. Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

 N.B.: SEE ALSO 0C004

 c. Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in radomes usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

 d. Bulk machinable siliconcarbide reinforced unfired ceramic, usable for nose tips usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

 e. Reinforced siliconcarbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

1C111 Propellants and constituent chemicals for propellants, not controlled in 1C011, as follows:

 

 a. Propulsive substances:

 

 1. Spherical aluminium powder, other than that specified in ML8.a., with particles of uniform diameter of less than 200 µm and an aluminium content of 97% by weight or more, if at least 10% of the total weight is made up of particles of less than 63 µm, according to ISO 2591:1988 or national equivalents;

 Technical Note:

 A particle size of 63 µm (ISO R565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E11).

 

 2. Metal fuels, other than that specified in ML8.a., in particle sizes of less than 60 µm, whether spherical, atomized, spheroidal, flaked or ground, consisting  97% by weight or more of any of the following:

 a. Zirconium;

 b. Beryllium;

 c. Magnesium; or

 d. Alloys of the metals specified by a. to c. above;

 

1C111 a. continued

 

Technical Note:

 The natural content of hafnium in the zirconium (typically 2% to 7%) is counted with the zirconium.

 

 3. Oxidiser substances usable in liquid propellant rocket engines as follows:

 a. Dinitrogen trioxide (CAS 10544737);

 b. Nitrogen dioxide (CAS 10102440)/dinitrogen tetroxide (CAS 10544726);

 c. Dinitrogen pentoxide (CAS 10102031);

 d. Mixed Oxides of Nitrogen (MON);

 Technical Note:

 Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2 ) that can be used in missile systems.  There are a range of compositions that can be denoted as MONi or MONij, where i and j are integers representing the percentage of Nitric Oxide in the mixture (e.g., MON3 contains 3% Nitric Oxide, MON25 25% Nitric Oxide.  An upper limit is MON40, 40% by weight).

 e. See ML8.d.10. for Inhibited Red Fuming Nitric Acid (IRFNA);

 f. See ML8.d.3. and 1C238 for

  compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;

 

4. Hydrazine derivatives as follows:

N.B.: SEE ALSO ML8.c.4.

 a. Trimethylhydrazine;

 b. Tetramethylhydrazine;

 c. N,N diallylhydrazine;

 d. Allylhydrazine;

 e. Ethylene dihydrazine;

 f. Monomethylhydrazine dinitrate;

 g. Unsymmetrical dimethylhydrazine nitrate;

 h. Hydrazinium azide;

 i. Dimethylhydrazinium azide;

 j. Hydrazinium dinitrate;

 k. Diimido oxalic acid dihydrazine;

 l. 2hydroxyethylhydrazine nitrate (HEHN);

 m. See ML8.c.4. for Hydrazinium perchlorate;

 n. Hydrazinium diperchlorate;

 o. Methylhydrazine nitrate (MHN);

 p. Diethylhydrazine nitrate (DEHN);

 q. 3,6dihydrazino tetrazine nitrate (1,4dihydrazine nitrate) (DHTN);

 

 b. Polymeric substances:

 1. Carboxyterminated polybutadiene (including carboxylterminated polybutadiene) (CTPB);

1C111 b. continued

 

 2. Hydroxyterminated polybutadiene (including hydroxylterminated polybutadiene) (HTPB), other than that specified in ML8.e.22.;

 3. Polybutadieneacrylic acid (PBAA);

 4. Polybutadieneacrylic acidacrylonitrile (PBAN);

5. Polytetrahydrofuran polyethylene glycol (TPEG);

Technical Note:

Polytetrahydrofuran polyethylene glycol (TPEG) is a block copolymer of poly 1,4Butanediol and polyethylene glycol (PEG).

 

 c. Other propellant additives and agents:

 1. See ML8.c.3. for  carboranes, decaboranes, pentaboranes and derivatives thereof;

 2. Triethylene glycol dinitrate (TEGDN) (CAS 111228);

 3. 2Nitrodiphenylamine;

 4. Trimethylolethane trinitrate (TMETN);

 5. Diethylene glycol dinitrate (DEGDN) (CAS 693210);

 6. Ferrocene derivatives as follows:

 a. See ML8.f.4.b. for catocene;

 b. Ethyl ferrocene;

 c. Propyl ferrocene (CAS 1273898);

 d. See ML8.f.4.d. for nbutyl ferrocene;

 e. Pentyl ferrocene (CAS 1274006);

 f. Dicyclopentyl ferrocene (CAS 20773288);

 g. Dicyclohexyl ferrocene;

 h. Diethyl ferrocene;

 i. Dipropyl ferrocene;

 j. Dibutyl ferrocene (CAS 1274084);

 k. Dihexyl ferrocene (CAS 93894598);

 l. Acetyl ferrocenes;

 m. See ML8.f.4.c. for ferrocene carboxylic acids;

 n. See ML8.f.4.a. for butacene;

 o. Other ferrocene derivatives usable as rocket propellant burning rate modifiers, not controlled in ML8.f.4.e.

 Note: For propellants and constituent chemicals for propellants not specified in 1C111, see ML8.

 

 

1C116 Maraging steels having an ultimate tensile strength of 1,500 MPa or greater, measured at 293 K (20°C), in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5 mm.

 N.B.: SEE ALSO 1C216.

 Technical Note:

 Maraging steels are iron alloys generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and agehardening of the alloy.

 

 

1C117 Tungsten, molybdenum and alloys of these metals in the form of uniform spherical or atomized particles of 500 micrometre diameter or less with a purity of 97% or greater for fabrication of rocket motor components usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 (i.e., heat shields, nozzle substrates, nozzle throats and thrust vector control surfaces).

 

 

1C118 Titaniumstabilised duplex stainless steel (TiDSS) having all of the following:

 

 a. Having all of the following characteristics:

 1. Containing 17.0 – 23.0 weight percent chromium and 4.5 – 7.0 weight percent nickel;

 2. Having a titanium content of greater than 0.10 weight percent; and

 3. A ferriticaustenitic microstructure (also referred to as a twophase microstructure) of which at least 10 percent is austenite by volume (according to ASTM E118187 or national equivalents); and

 

 b. Having any of the following forms:

 1. Ingots or bars having a size of 100 mm or more in each dimension;

 2. Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or

 3. Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.

 

 

1C202 Alloys, not controlled in 1C002.b.3. or .b.4., as follows:

 

 a. Aluminium alloys having both of the following characteristics:

 1. ‘Capable of’ an ultimate tensile strength of 460 MPa or more at 293 K (20°C); and

 2. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;

 

 b. Titanium alloys having both of the following characteristics:

 1. ‘Capable of’ an ultimate tensile strength of 900 MPa or more at 293 K (20°C); and

 2. In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.

 

 Technical Note:

 The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment.

 

 

1C210 ‘Fibrous or filamentary materials’ or prepregs, not controlled in 1C010.a., b. or e., as follows:

 

 a. Carbon or aramid ‘fibrous or filamentary materials’ having either of the following characteristics:

 

 

1C210 a. continued

 

 1. A “specific modulus” of 12.7 x 106 m or greater; or

 2. A “specific tensile strength” of 235 x 103 m or greater;

  

 Note: 1C210.a. does not control aramid ‘fibrous or filamentary materials’ having 0.25 percent or more by weight of an ester based fibre surface modifier;

 

 b. Glass ‘fibrous or filamentary materials’ having both of the following characteristics:

 1. A “specific modulus” of 3.18 x 106 m or greater; and

 2. A “specific tensile strength” of 76.2 x 103 m or greater;

 

 c. Thermoset resin impregnated continuous “yarns”, “rovings”, “tows” or “tapes” with a width of 15 mm or less (prepregs), made from carbon or glass ‘fibrous or filamentary materials’ specified in 1C210.a. or b.

 Technical Note:

 The resin forms the matrix of the composite.

 

 Note: In 1C210, ‘fibrous or filamentary materials’ is  restricted to continuous “monofilaments”, “yarns”, “rovings”, “tows” or “tapes”.

 

 

1C216 Maraging steel, other than that specified in 1C116, ‘capable of’ an ultimate tensile strength of 2,050 MPa or more, at 293 K (20oC).

 

 Note: 1C216 does not control forms in which all linear dimensions are 75 mm or less.

 Technical Note:

 The phrase maraging steel ‘capable of’ encompasses maraging steel before or after heat treatment.

 

1C225 Boron enriched in the boron10 (10B) isotope to greater than its natural isotopic

 abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.

 

 Note: In 1C225 mixtures containing boron include boron loaded materials.

 Technical Note:

 The natural isotopic abundance of boron10 is approximately 18.5 weight per cent (20 atom per cent).

 

 

1C226 Tungsten, tungsten carbide, and alloys containing more than 90% tungsten by weight, having both of the following characteristics:

 

 a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; and

 b. A mass greater than 20 kg.

 Note: 1C226 does not control manufactures specially designed as weights or gammaray collimators.

 

1C227 Calcium having both of the following characteristics:

 

 a. Containing less than 1,000 parts per million by weight of metallic impurities other than magnesium; and

 b. Containing less than 10 parts per million by weight of boron.

 

 

1C228 Magnesium having both of the following characteristics:

 

 a. Containing less than 200 parts per million by weight of metallic impurities other than calcium; and

 b. Containing less than 10 parts per million by weight of boron.

 

 

1C229 Bismuth having both of the following characteristics:

 

 a. A purity of 99.99% or greater by weight; and

 b. Containing less than 10 parts per million by weight of silver.

 

 

1C230 Beryllium metal, alloys containing more than 50% beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing.

 

 Note: 1C230 does not control the following:

  a. Metal windows for Xray machines, or for borehole logging devices;

  b. Oxide shapes in fabricated or semifabricated forms specially designed for electronic component parts or as substrates for electronic circuits;

  c. Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines.

 

 

1C231 Hafnium metal, alloys containing more than 60% hafnium by weight, hafnium compounds containing more than 60% hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.

 

 

1C232 Helium3 (3He), mixtures containing helium3, and products or devices containing any of the foregoing.

 

 Note: 1C232 does not control a product or device containing less than 1 g of helium3.

 

 

1C233 Lithium enriched in the lithium6 (6Li) isotope to greater than its natural isotopic

 abundance, and products or devices containing enriched lithium, as follows:  elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.

 

 Note: 1C233 does not control thermoluminescent dosimeters.

 Technical Note:

 The natural isotopic abundance of lithium6 is approximately 6.5 weight per cent (7.5 atom per cent).

 

 

1C234 Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows:  metal, alloys containing more than 50% zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing.

 

 Note: 1C234 does not control zirconium in the form of foil having a thickness of 0.10 mm or less.

 

 

1C235 Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.

 

 Note: 1C235 does not control a product or device containing less than 1.48 x 103 GBq (40 Ci) of tritium.

 

 

1C236 Alphaemitting radionuclides having an alpha halflife of 10 days or greater but less than 200 years, in the following forms:

 

 a. Elemental;

 b. Compounds having a total alpha activity of 37 GBq/kg (1 Ci/kg) or greater;

 c. Mixtures having a total alpha activity of 37 GBq/kg (1 Ci/kg) or greater;

 d. Products or devices containing any of the foregoing.

 

 Note: 1C236 does not control a product or device containing less than 3.7 GBq (100 millicuries) of alpha activity.

 

 

1C237 Radium226 (226Ra), radium226 alloys, radium226 compounds, mixtures containing               radium226, manufactures therof, and products or devices containing any of the foregoing.

 

 Note: 1C237 does not control the following:

  a. Medical applicators;

  b. A product or device containing less than 0.37 GBq (10 millicuries) of radium226.

 

 

1C238 Chlorine trifluoride (ClF3).

1C239 High explosives, not controlled in ML8, or substances or mixtures containing more than 2% by weight thereof, with a crystal density greater than 1.8 g/cm3 and having a detonation velocity greater than 8,000 m/s.

 

 

1C240 Nickel powder and porous nickel metal, not controlled in 0C005, as

 follows:

 

 a. Nickel powder having both of the following characteristics:

 1. A nickel purity content of 99.0% or greater by weight; and

 2. A mean particle size of less than 10 micrometres measured by American Society for Testing and Materials (ASTM) B330 standard;

 

 b. Porous nickel metal produced from materials specified in 1C240.a.

 

 Note: 1C240 does not control the following:

  a. Filamentary nickel powders;

  b. Single porous nickel sheets with an area of 1,000 cm2 per sheet or less.

 

 Technical Note:

 1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure.

 

 

1C350 Chemicals, which may be used as precursors for toxic chemical agents, as follows, and “chemical mixtures” containing one or more thereof:

 N.B.: SEE ALSO ML7 AND 1C450.

 

 1. Thiodiglycol (111488);

 2. Phosphorus oxychloride (10025873);

 3. Dimethyl methylphosphonate (756796);

 4. See ML7.b.1. for methyl phosphonyl difluoride (676993);

 5. Methyl phosphonyl dichloride (676971);

 6. Dimethyl phosphite (DMP) (868859);

 7. Phosphorus trichloride (7719122);

 8. Trimethyl phosphite (TMP) (121459);

 9. Thionyl chloride (7719097);

 10. 3Hydroxy1methylpiperidine (3554743);

 11. N,NDiisopropyl(beta)aminoethyl chloride (96797);

 12. N,NDiisopropyl(beta)aminoethane thiol (5842079);

 13. 3Quinuclidinol (1619347);

 14. Potassium fluoride (7789233);

 15. 2Chloroethanol (107073);

 16. Dimethylamine (124403);

 17. Diethyl ethylphosphonate (78386);

 18. DiethylN,Ndimethylphosphoramidate (2404037);

 19. Diethyl phosphite (762049);

 20. Dimethylamine hydrochloride (506592);

 21. Ethyl phosphinyl dichloride (1498404);

1C350 continued

 

 22. Ethyl phosphonyl dichloride (1066508);

 23. See ML7.b.1. for ethyl phosphonyl difluoride (753980);

 24. Hydrogen fluoride (7664393);

 25. Methyl benzilate (76891);

 26. Methyl phosphinyl dichloride (676835);

 27. N,NDiisopropyl(beta)amino ethanol (96800);

 28. Pinacolyl alcohol (464073);

 29. See ML7.b.2. for OEthyl2diisopropylaminoethyl methyl phosphonite (QL) (57856118);

 30. Triethyl phosphite (122521);

 31. Arsenic trichloride (7784341);

 32. Benzilic acid (76937);

 33. Diethyl methylphosphonite (15715410);

 34. Dimethyl ethylphosphonate (6163753);

 35. Ethyl phosphinyl difluoride (430784);

 36. Methyl phosphinyl difluoride (753593);

 37. 3Quinuclidone (3731382);

 38. Phosphorus pentachloride (10026138);

 39. Pinacolone (75978);

 40. Potassium cyanide (151508);

 41. Potassium bifluoride (7789299);

 42. Ammonium hydrogen fluoride or ammonium bifluoride (1341497);

 43. Sodium fluoride (7681494);

 44. Sodium bifluoride (1333831);

 45. Sodium cyanide (143339);

 46. Triethanolamine (102716);

 47. Phosphorus pentasulphide (1314803);

 48. Diisopropylamine (108189);

 49. Diethylaminoethanol (100378);

 50. Sodium sulphide (1313822);

 51. Sulphur monochloride (10025679);

 52. Sulphur dichloride (10545990);

 53. Triethanolamine hydrochloride (637398);

 54. N,NDiisopropyl(Beta)aminoethyl chloride hydrochloride (4261681);

 55. Methylphosphonic acid (993135);

 56. Diethyl methylphosphonate (683089);

 57. N,NDimethylaminophosphoryl dichloride or                                          N,Ndimethyl phosphoramidic dichloride (677430);

 58. Triisopropyl phosphite (116176);

 59. Ethyldiethanolamine (139877);

 60. O,ODiethyl phosphorothioate (2465658);

 61. O,ODiethyl phosphorodithioate (298066);

 62. Sodium hexafluorosilicate (16893859);

 63. Methylphosphonothioic dichloride (676982);

 64. Thiophosphoryl chloride (3982910);

 65. Oxalyl chloride (79378).

 

1C350 continued

 

 Note 1: For exports to “States not Party to the Chemical Weapons Convention”, 1C350 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 10% by the weight of the mixture.

 

 Note 2: For exports to “States Party to the Chemical Weapons Convention”, 1C350 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 30% by the weight of the mixture.

 

 Note 3: 1C350 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C350 .2, .6, .7, .8, .9, .10, .14, .15, .16, .19, .20, .24, .25, .30, .37, .38, .39, .40, .41, .42, .43, .44, .45, .46, .47, .48, .49, .50, .51, .52, .53, .58, .59, .60, .61, .62, .64 and .65 in which no individually specified chemical constitutes more than 30% by the weight of the mixture.

 

 Note 4: 1C350 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

 N.B.: This exemption does not apply to chemicals 1C350.4, .23 and .29 (see Note 5 of ML7).

 

 

1C351 Human pathogens, zoonoses and “toxins”, as follows:

 

 a. Viruses, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Chikungunya virus;

 2. CongoCrimean haemorrhagic fever virus;

 3. Dengue fever virus;

 4. Eastern equine encephalitis virus;

 5. Ebola virus;

 6. Hantaan virus;

 7. Junin virus;

 8. Lassa fever virus;

 9. Lymphocytic choriomeningitis virus;

 10. Machupo virus;

 11. Marburg virus;

 12. Monkey pox virus;

 13. Rift Valley fever virus;

 14. Tickborne encephalitis virus (Russian SpringSummer encephalitis virus);

 15. Variola virus;

1C351 continued

 

 16. Venezuelan equine encephalitis virus;

 17. Western equine encephalitis virus;

 18. White pox;

 19. Yellow fever virus;

 20. Japanese encephalitis virus;

 21. Kyasanur Forest virus;

 22. Louping ill virus;

 23. Murray Valley encephalitis virus;

 24. Omsk haemorrhagic fever virus;

 25. Oropouche virus;

 26. Powassan virus;

 27. Rocio virus;

 28. St Louis encephalitis virus;

 29. Hendra virus (Equine morbillivirus);

 30. South American haemorrhagic fever (Sabia, Flexal, Guanarito);

 31. Pulmonary & renal syndromehaemorrhagic fever viruses

  (Seoul, Dobrava, Puumala, Sin Nombre);

 32. Nipah virus.

 

 b. Rickettsiae, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Coxiella burnetii;

 2. Bartonella quintana (Rochalimaea quintana, Rickettsia quintana);

 3. Rickettsia prowasecki;

 4. Rickettsia rickettsii.

 

 c. Bacteria, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Bacillus anthracis;

 2. Brucella abortus;

 3. Brucella melitensis;

 4. Brucella suis;

 5. Chlamydia psittaci;

5.         Clostridium botulinum;

 7. Francisella tularensis;

 8. Burkholderia mallei (Pseudomonas mallei);

 9. Burkholderia pseudomallei (Pseudomonas pseudomallei);

 10. Salmonella typhi;

 11. Shigella dysenteriae;

 12. Vibrio cholerae;

 13. Yersinia pestis;

 14. Clostridium perfringens epsilon toxin producing types;

 15. Enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing serotypes.

 

1C351 continued

 

 d. “Toxins”, as follows, and “subunit of toxins” thereof:

 1. Botulinum toxins;

 2. Clostridium perfringens toxins;

 3. Conotoxin;

 4. Ricin;

 5. Saxitoxin;

 6. Shiga toxin;

 7. Staphylococcus aureus toxins;

 8. Tetrodotoxin;

 9. Verotoxin and shigalike ribosome inactivating proteins;

 10. Microcystin (Cyanginosin);

 11. Aflatoxins;

 12. Abrin;

 13. Cholera toxin;

 14. Diacetoxyscirpenol toxin;

 15. T2 toxin;

 16. HT2 toxin;

 17. Modeccin;

 18. Volkensin;

 19. Viscum album Lectin 1 (Viscumin).

 

 Note: 1C351.d. does not control botulinum toxins or conotoxins in product form meeting all of the following criteria:

 1. Are pharmaceutical formulations designed for human administration in the treatment of medical conditions;

  2. Are prepackaged for distribution as medical products;

  3. Are authorised by a state authority to be marketed as medical products.

 

 e. Fungi, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Coccidioides immitis;

 2. Coccidioides posadasii.

 

Note: 1C351 does not control “vaccines” or “immunotoxins”.

 

 

1C352 Animal pathogens, as follows:

 

 a. Viruses, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. African swine fever virus;

 2. Avian influenza virus, which are:

 a. Uncharacterised; or

1C352 continued

 

 b. Defined in Annex I(2) EC Directive 2005/94/EC (O.J. L.10 14.1.2006 p.16) as having high pathogenicity, as follows:

 1. Type A viruses with an IVPI (intravenous pathogenicity index) in 6 week old chickens of greater than 1.2; or

 2. Type A viruses of the subtypes H5 or H7 with genome sequences codified for multiple basic amino acids at the cleavage site of  the haemagglutinin  molecule similar to that observed for other HPAI viruses, indicating that the haemagglutinin molecule can be cleaved by a host ubiquitous protease;

 3. Bluetongue virus;

 4. Foot and mouth disease virus;

 5. Goat pox virus;

 6. Porcine herpes virus (Aujeszky’s disease);

 7. Swine fever virus (Hog cholera virus);

 8. Lyssa virus;

 9. Newcastle disease virus;

 10. Peste des petits ruminants virus;

 11. Porcine enterovirus type 9 (swine vesicular disease virus);

 12. Rinderpest virus;

 13. Sheep pox virus;

 14. Teschen disease virus;

 15. Vesicular stomatitis virus;

 16. Lumpy skin disease virus;

 17. African horse sickness virus.

 

 b. Mycoplasmas, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Mycoplasma mycoides subspecies mycoides SC (small colony);

 2. Mycoplasma capricolum subspecies capripneumoniae.

 

 Note: 1C352 does not control “vaccines”.

 

 

1C353 Genetic elements and genetically modified organisms, as follows:

 

 a. Genetically modified organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity of organisms specified in 1C351.a., 1C351.b., 1C351.c, 1C351.e., 1C352 or 1C354;

 

 b. Genetically modified organisms or genetic elements that contain nucleic acid sequences coding for any of the “toxins” specified in 1C351.d. or “subunits of toxins” thereof.

 

 Technical Notes:

1. Genetic elements include, inter alia, chromosomes, genomes, plasmids, transposons and vectors whether genetically modified or unmodified.

 

1C353 continued

 

2. Nucleic acid sequences associated with the pathogenicity of any of the microorganisms specified in 1C351.a., 1C351.b., 1C351.c., 1C351.e., 1C352 or 1C354 means any sequence specific to the specified  microorganism that:

 a. In itself or through its transcribed or translated products represents a significant hazard to human, animal or plant health; or

 b. Is known to enhance the ability of a specified microorganism, or any other organism into which it may be inserted or otherwise integrated, to cause serious harm to humans, animals or plant health.

 

 Note: 1C353 does not apply to nucleic acid sequences associated with the pathogenicity of enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing strains, other than those coding for the verotoxin, or for its subunits.

 

 

1C354 Plant pathogens, as follows:

 

a. Viruses, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Potato Andean latent tymovirus;

 2. Potato spindle tuber viroid.

 

b. Bacteria, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Xanthomonas albilineans;

 2. Xanthomonas campestris pv. citri including strains referred to as Xanthomonas campestris pv. citri types A,B,C,D,E or otherwise classified as Xanthomonas citri, Xanthomonas campestris pv. aurantifolia or Xanthomonas campestris pv. citrumelo;

 3. Xanthomonas oryzae pv. Oryzae (Pseudomonas campestris pv. Oryzae);

 4. Clavibacter michiganensis subsp. Sepedonicus (Corynebacterium michiganensis subsp. Sepedonicum or Corynebacterium Sepedonicum);

 5. Ralstonia solanacearum Races 2 and 3 (Pseudomonas solanacearum Races 2 and 3 or Burkholderia solanacearum Races 2 and 3).

 

 c. Fungi, whether natural, enhanced or modified, either in the form of “isolated live cultures” or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

 1. Colletotrichum coffeanum var. virulans (Colletotrichum kahawae);

 2. Cochliobolus miyabeanus (Helminthosporium oryzae);

 3. Microcyclus ulei (syn. Dothidella ulei);

 4. Puccinia graminis (syn. Puccinia graminis f. sp. tritici);

 5. Puccinia striiformis (syn. Puccinia glumarum);

 6. Magnaporthe grisea (pyricularia grisea/pyricularia oryzae).

 

 

1C450 Toxic chemicals and toxic chemical precursors, as follows, and “chemical mixtures” containing one or more thereof:

 N.B.: SEE ALSO 1C350, 1C351.d. AND ML7.

 

 a. Toxic chemicals, as follows:

 

 1. Amiton: O,ODiethyl S[2(diethylamino)ethyl] phosphorothiolate (78535) and corresponding alkylated or protonated salts;

 2. PFIB: 1,1,3,3,3Pentafluoro2(trifluoromethyl)1propene (382218);

 3. See ML7.b.3. for BZ: 3Quinuclidinyl benzilate (6581062);

 4. Phosgene: Carbonyl dichloride (75445);

 5. Cyanogen chloride (506774);

 6. Hydrogen cyanide (74908);

 7. Chloropicrin: Trichloronitromethane (76062);

 

 Note 1: For exports to “States not Party to the Chemical Weapons Convention”, 1C450 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C450.a.1. and .a.2. in which no individually specified chemical constitutes more than 1% by the weight of the mixture.

 

 Note 2: For exports to “States Party to the Chemical Weapons Convention”, 1C450 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C450.a.1. and  .a.2. in which no individually specified chemical constitutes more than 30% by the weight of the mixture.

 

 Note 3: 1C450 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C450.a.4., .a.5., .a.6. and .a.7. in which no individually specified chemical constitutes more than 30% by the weight of the mixture.

 

Note 4: 1C450 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

 

 b. Toxic chemical precursors, as follows:

 

 1. Chemicals, not controlled in the Munitions List or in 1C350, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms, including:

 

a.              diphenyl methylphosphonate (7526263);

b. phosphonic acid, methyl, methyl 3(trimethoxysilyl) propyl ester (67812173);

c.              phosphonic acid, methyl, monoammonium salt (34255873);

d. phosphonic acid, methyl, monomethyl ester, monosodium salt (73750693);

e.              phosphonothioic dichloride, ethyl (993431);

f. phosphonic acid, methyl, bis(3(trimethoxysilyl)propyl) ester (67812184);

1C450 b. continued

 

g. phosphonic acid, methyl, compd. with (aminoiminomethyl) urea (1:1) (84402584);

h. phosphonic acid, methyl, (5ethyl2methyl1,3,2dioxaphosphorinan5yl) methyl methyl ester, Poxide)
(41203810);

i. phosphonic acid, methyl, bis((5ethyl2methyl1,3,2dioxaphosphorinan5yl) methyl ester, P,P’dioxide) (42595459).

 

 Note: 1C450.b.1. does not control Fonofos: OEthyl Sphenyl ethylphosphonothiolothionate (944229);

 

2. N,NDialkyl [methyl, ethyl or propyl (normal or iso)] phosphoramidic dihalides, other than N,NDimethylaminophosphoryl dichloride or N,Ndimethyl phosphoramidic dichloride (677430);

N.B.: See 1C350.57. for N,Ndimethylaminophosphoryl dichloride or N,Ndimethyl phosphoramidic dichloride (677430).

 3. Dialkyl [methyl, ethyl or propyl (normal or iso)] N,Ndialkyl [methyl, ethyl or propyl (normal or iso)]phosphoramidates, other than DiethylN,Ndimethylphosphoramidate (2404037) which is specified in 1C350;

 4. N,NDialkyl [methyl, ethyl or propyl (normal or iso)] aminoethyl2chlorides and corresponding protonated salts, other than N,NDiisopropyl(beta)aminoethyl chloride (96797) or N,NDiisopropyl(beta)aminoethyl chloride hydrochloride (4261681) which are specified in 1C350;

 5. N,NDialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane2ols and corresponding protonated salts, other than N,NDiisopropyl(beta)aminoethanol (96800) and N,NDiethylaminoethanol (100378) which are specified in 1C350;

 

Note: 1C450.b.5. does not control the following:

  a. N,NDimethylaminoethanol (108010) and corresponding protonated salts;

  b. Protonated salts of N,NDiethylaminoethanol (100378);

 6. N,NDialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane2thiols and corresponding protonated salts, other than N,NDiisopropyl(beta)aminoethane thiol (5842079) which is specified in 1C350;

 7. See 1C350 for ethyldiethanolamine (139877);

 8. Methyldiethanolamine (105599).

 

1C450 b. continued

 

 Note 1: For exports to “States not Party to the Chemical Weapons Convention”, 1C450 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 10% by the weight of the mixture.

 

 Note 2: For exports to “States Party to the Chemical Weapons Convention”, 1C450 does not control “chemical mixtures” containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 30% by the weight of the mixture.

 

 Note 3: 1C450 does not control chemical mixtures” containing the chemical specified in entry 1C450.b.8. in which the specified chemical constitutes no more than 30% by the weight of the mixture.

 

 Note 4: 1C450 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use.

 

 

1D Software

 

1D001 “Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 1B001 to 1B003.

 

 

1D002 “Software” for the “development” of organic “matrix”, metal “matrix” or carbon

 “matrix” laminates or “composites”.

 

 

1D003 “Software” specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c.

 

 

1D101 “Software” specially designed or modified for the “use” of goods specified in 1B101.

 

 

1D103 “Software” specially designed for analysis of reduced observables such as radar

 reflectivity, ultraviolet/infrared signatures and acoustic signatures.

 

 

1D201 “Software” specially designed for the “use” of goods specified in 1B201.

 

 

1E Technology

 

1E001 “Technology” according to the General Technology Note for the “development”

 or “production” of equipment or materials specified in 1A001.b., 1A001.c., 1A002 to 1A005, 1B or 1C.

 

1E002 Other “technology” as follows:

 

 a. “Technology” for the “development” or “production” of polybenzothiazoles or polybenzoxazoles;

 

 b. “Technology” for the “development” or “production” of fluoroelastomer compounds containing at least one vinylether monomer;

 

 c. “Technology” for the design or “production” of the following base materials or non“composite” ceramic materials:

 

 1. Base materials having all of the following:

 a. Any of the following compositions:

 1. Single or complex oxides of zirconium and complex oxides of silicon or aluminium;

 2. Single nitrides of boron (cubic crystalline forms);

 3. Single or complex carbides of silicon or boron; or

 4. Single or complex nitrides of silicon;

 b. Any of the following total metallic impurities (excluding intentional additions):

 1. Less than 1,000 ppm for single oxides or carbides; or

 2. Less than 5,000 ppm for complex compounds or single nitrides; and

 c. Being any of the following:

 1. Zirconia with an average particle size equal to or less than 1 µm and no more than 10% of the particles larger than 5 µm;

 2. Other base materials with an average particle size equal to or less than 5 µm and no more than 10% of the particles larger than 10 µm; or

 3. Having all of the following:

 a. Platelets with a length to thickness ratio exceeding 5;

 b. Whiskers with a length to diameter ratio exceeding 10 for diameters less than 2 µm; and

 c. Continuous or chopped fibres less than 10 µm in diameter;

 

 2. Non“composite” ceramic materials composed of the materials specified in 1E002.c.1;

 Note: 1E002.c.2. does not control “technology” for the design or production of abrasives.

 

 d. “Technology” for the “production” of aromatic polyamide fibres;

 

 e. “Technology” for the installation, maintenance or repair of materials specified in 1C001;

1E002 continued

 

 f. “Technology” for the repair of “composite” structures, laminates or materials specified in 1A002, 1C007.c. or 1C007.d.

 Note: 1E002.f. does not control “technology” for the repair of “civil aircraft” structures using carbon “fibrous or filamentary materials” and epoxy resins, contained in aircraft manufacturers’ manuals.

 

g. ‘Libraries (parametric technical databases)’ specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c.

Technical Note:

For the purpose of 1E002.g., ‘library (parametric technical database)’ means a collection of technical information, reference to which may enhance the performance of relevant equipment or systems.

 

 

1E101 “Technology” according to the General Technology Note for the “use” of goods specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1C107, 1C111 to 1C118, 1D101 or 1D103.

 

 

1E102 “Technology” according to the General Technology Note for the “development” of “software” specified in 1D001, 1D101 or 1D103.

 

 

1E103 “Technology” for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the “production” of “composites” or partially processed “composites”.

 

 

1E104 “Technology” relating to the “production” of pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1,573 K (1,300°C) to 3,173 K (2,900°C) temperature range at pressures of 130 Pa to 20 kPa.

 Note: 1E104 includes “technology” for the composition of precursor gases, flowrates and process control schedules and parameters.

 

 

1E201 “Technology” according to the General Technology Note for the “use” of goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B233, 1C002.b.3. or .b.4., 1C010.b., 1C202, 1C210, 1C216, 1C225 to 1C240 or 1D201.

 

 

1E202 “Technology” according to the General Technology Note for the “development” or “production” of goods specified in 1A007, 1A202 or 1A225 to 1A227.

 

1E203 “Technology” according to the General Technology Note for the “development” of “software” specified in 1D201.

 

CATEGORY 2 – MATERIALS PROCESSING

 

 

 

2A Systems, Equipment and Components

 

 N.B.: For quiet running bearings, see ML9.g.

 

 

2A001 Antifriction bearings and bearing systems, as follows, and components therefor:

 

 Note: 2A001 does not control balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse.

 

 a. Ball bearings and solid roller bearings having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 4 (or ANSI/ABMA Std 20 Tolerance Class ABEC7 or RBEC7, or other national equivalents), or better, and having both rings and rolling elements (ISO 5593), made from monel or beryllium;

 Note: 2A001.a. does not control tapered roller bearings.

 

 b. Other ball bearings and solid roller bearings having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC9 or RBEC9, or other national equivalents), or better;

 Note: 2A001.b. does not control tapered roller bearings.

 

 c. Active magnetic bearing systems using any of the following:

 1. Materials with flux densities of 2.0 T or greater and yield strengths greater than 414 MPa;

 2. Allelectromagnetic 3D homopolar bias designs for actuators; or

 3. High temperature (450 K (177°C) and above) position sensors.

 

 

2A225 Crucibles made of materials resistant to liquid actinide metals, as follows:

 

 a. Crucibles having both of the following characteristics:

 1. A volume of between 150 cm3 and 8,000 cm3; and

 2. Made of or coated with any of the following materials, having a purity of 98% or greater by weight:

 a. Calcium fluoride (CaF2);

 b. Calcium zirconate (metazirconate) (CaZrO3);

 c. Cerium sulphide (Ce2S3);

 d. Erbium oxide (erbia) (Er2O3);

 e. Hafnium oxide (hafnia) (HfO2);

 f. Magnesium oxide (MgO);

 g. Nitrided niobiumtitaniumtungsten alloy (approximately 50% Nb, 30% Ti, 20% W);

2A225 a. continued

 h. Yttrium oxide (yttria) (Y2O3); or

 i. Zirconium oxide (zirconia) (ZrO2);

 

 b. Crucibles having both of the following characteristics:

 1. A volume of between 50 cm3 and 2,000 cm3; and

 2. Made of or lined with tantalum, having a purity of 99.9% or greater by weight;

 

 c. Crucibles having all of the following characteristics:

 1. A volume of between 50 cm3 and 2,000 cm3;

 2. Made of or lined with tantalum, having a purity of 98% or greater by weight; and

 3. Coated with tantalum carbide, nitride, boride, or any combination thereof.

 

 

2A226 Valves having all of the following characteristics:

 

 a. A ‘nominal size’ of 5 mm or greater;

 b. Having a bellows seal; and

 c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60% nickel by weight.

 

 Technical Note:

 For valves with different inlet and outlet diameters, the ‘nominal size’ in 2A226 refers to the smallest diameter.

 

 

2B Test, Inspection and Production Equipment

 

 Technical Notes:

 1. Secondary parallel contouring axes, (e.g., the waxis on horizontal boring mills or a secondary rotary axis the centre line of which is parallel to the primary rotary axis) are not counted in the total number of contouring axes.  Rotary axes need not rotate over 360°.  A rotary axis can be driven by a linear device (e.g. a screw or a rackandpinion).

 2. For the purposes of 2B, the number of axes which can be coordinated simultaneously for “contouring control” is the number of axes along or around which, during processing of the workpiece, simultaneous and interrelated motions are performed between the workpiece and a tool.  This does not include any additional axes along or around which other relative movements within the machine are performed such as:

a. Wheeldressing systems in grinding machines;

b. Parallel rotary axes designed for mounting of separate workpieces;

c. Colinear rotary axes designed for manipulating the same workpiece by holding it in a chuck from different ends.

 3. Axis nomenclature shall be in accordance with International Standard ISO 841, ‘Numerical Control Machines Axis and Motion Nomenclature’.

 4. For the purposes of 2B001 to 2B009 a “tilting spindle” is counted as a rotary axis.

2B continued

 

 5. Stated positioning accuracy derived from measurements made according to ISO 230/2 (1988)[1] or national equivalents may be used for each machine tool model as an alternative to individual machine tests. Stated positioning accuracy means the accuracy value provided to the competent authorities of the Member State in which the exporter is established as representative of the accuracy of a specific machine model.

 

Determination of Stated Positioning Accuracy

a. Select five machines of a model to be evaluated;

b. Measure the linear axis accuracies according to ISO 230/2 (1988)[2];

c. Determine the Avalues for each axis of each machine. The method of calculating the Avalue is described in the ISO standard;

d. Determine the mean value of the Avalue of each axis. This mean value  becomes the stated value of each axis for the model (Âx    Ây...);

e. Since the Category 2 list refers to each linear axis there will be as many stated values as there are linear axes;

f. If any axis of a machine model not controlled by 2B001.a. to 2B001.c. or 2B201 has a stated accuracy  of 6 microns for grinding machines and 8 microns for milling and turning machines or better, the manufacturer should be required to reaffirm the accuracy level once every eighteen months.

 

 

2B001 Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or “composites”, which, according to the manufacturer’s technical specification, can be equipped with electronic devices for “numerical control”, and specially designed components as follows:

 N.B.: SEE ALSO 2B201.

 

 Note 1: 2B001 does not control special purpose machine tools limited to the manufacture of gears.  For such machines see 2B003.

 Note 2: 2B001 does not control special purpose machine tools limited to the manufacture of any of the following:

  a. Crankshafts or cam shafts;

  b. Tools or cutters;

  c. Extruder worms;or

  d. Engraved or facetted jewellery parts.

 Note 3: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g. a turning machine with milling capability), must be evaluated against each applicable entry 2B001.a., b. or c.

 

N.B.: For optical finishing machines, see 2B002.

 

2B001 continued

 

 a. Machine tools for turning having all of the following:

1. Positioning accuracy with “all compensations available” equal to or less (better) than 6 µm according to ISO 230/2 (1988)[3] or national equivalents along any linear axis; and

2. Two or more axes which can be coordinated simultaneously for “contouring control”;

 Note: 2B001.a. does not control turning machines specially designed for producing contact lenses, having all of the following:

1. Machine controller limited to using ophthalmic based software for part programming data input; and

2. No vacuum chucking.

 

 b. Machine tools for milling, having any of the following:

 1. Having all of the following:

 a. Positioning accuracy with “all compensations available” equal to or less (better) than 6 µm according to ISO 230/2 (1988)[4] or national equivalents along any linear axis; and

 b. Three linear axes plus one rotary axis which can be coordinated simultaneously for “contouring control”;

 2. Five or more axes which can be coordinated simultaneously for “contouring control”;

 3. A positioning accuracy for jig boring machines, with “all compensations available”, equal to or less (better) than 4 µm according to ISO 230/2 (1988)[5] or national equivalents along any linear axis; or

 4. Fly cutting machines having all of the following:

 a. Spindle “runout” and “camming” less (better) than 0.0004 mm TIR; and

 b. Angular deviation of slide movement (yaw, pitch and roll) less (better) than 2 seconds of arc, TIR over 300 mm of travel.

 

 c. Machine tools for grinding, having any of the following:

 1. Having all of the following:

 a. Positioning accuracy with “all compensations available” equal to or less (better) than 4 µm according to ISO 230/2 (1988)[6] or national equivalents along any linear axis; and

 b. Three or more axes which can be coordinated simultaneously for “contouring control”; or

 2. Five or more axes which can be coordinated simultaneously for “contouring control”;

2B001 c. continued

 

 Note: 2B001.c. does not control grinding machines, as follows:

  a. Cylindrical external, internal, and externalinternal grinding machines, having all of the following:

  1. Limited to cylindrical grinding; and

  2. Limited to a maximum workpiece capacity of 150 mm outside diameter or length.

  b. Machines designed specifically as jig grinders that do not have a zaxis or a waxis, with a positioning accuracy with “all compensations available” less (better) than 4 µm according to ISO 230/2 (1988)[1] or national equivalents.

  c. Surface grinders.

 

 d. Electrical discharge machines (EDM) of the nonwire type which have two or more rotary axes which can be coordinated simultaneously for “contouring control”;

 

 e. Machine tools for removing metals, ceramics or “composites”, having all of the following characteristics:

 1. Removing material by means of any of the following:

 a. Water or other liquid jets, including those employing abrasive additives;

 b. Electron beam; or

 c. “Laser” beam; and

 2. Having two or more rotary axes and all of the following:

 a. Can be coordinated simultaneously for “contouring control”; and

 b. A positioning accuracy of less (better) than 0.003°;

 

 f. Deepholedrilling machines and turning machines modified for deepholedrilling, having a maximum depthofbore capability exceeding  5 m and specially designed components therefor.

 

2B002 Numerically controlled optical finishing machine tools equipped for selective material removal to produce nonspherical optical surfaces having all of the following characteristics:

 a. Finishing the form to less (better) than 1.0 µm;

 b. Finishing to a roughness less (better) than 100 nm rms;

 c. Four or more axes which can be coordinated simultaneously for “contouring control”; and

 d. Using any of the following processes:

1. Magnetorheological finishing (‘MRF’);

2. Electrorheological finishing (‘ERF’);

3. Energetic particle beam finishing;

4. ‘Inflatable membrane tool finishing’; or

5. ‘Fluid jet finishing’.

2B002 continued

 

 Technical Notes:

 For the purposes of 2B002:

1. ‘MRF’ is a material removal process using an abrasive magnetic fluid whose viscosity is controlled by a magnetic field.

2. ‘ERF’ is a removal process using an abrasive fluid whose viscosity is controlled by an electric field.

3. ‘Energetic particle beam finishing’ uses Reactive Atom Plasmas (RAP) or ionbeams to selectively remove material.

4. ‘Inflatable membrane tool finishing’ is a process that uses a pressurized membrane that deforms to contact the workpiece over a small area.

5. ‘Fluid jet finishing’ makes use of a fluid stream for material removal.

 

 

2B003 “Numerically controlled” or manual machine tools, and specially designed components, controls and accessories therefor, specially designed for the shaving, finishing, grinding or honing of hardened (Rc = 40 or more) spur, helical and doublehelical gears with a pitch diameter exceeding 1,250 mm and a face width of 15% of pitch diameter or larger finished to a quality of AGMA 14 or better (equivalent to ISO 1328 class 3).

 

 

2B004 Hot “isostatic presses” having all of the following, and specially designed components and accessories therefor:

 N.B.: SEE ALSO 2B104 AND 2B204.

 

 a. A controlled thermal environment within the closed cavity and a chamber cavity with an inside diameter of 406 mm or more; and

 b. Having any of the following:

 1. A maximum working pressure exceeding 207 MPa;

 2. A controlled thermal environment exceeding 1,773 K (1,500°C); or

 3. A facility for hydrocarbon impregnation and removal of resultant gaseous degradation products.

 

 Technical Note:

 The inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.

 N.B.: For specially designed dies, moulds and tooling see 1b003, 9b009 and ML18.

 

 

2B005 Equipment specially designed for the deposition, processing and inprocess control of inorganic overlays, coatings and surface modifications, as follows, for nonelectronic substrates, by processes shown in the Table and associated Notes following 2E003.f., and specially designed automated handling, positioning, manipulation and control components therefor:

 

 a. Chemical vapour deposition (CVD) production equipment having all of the following:

 N.B.: SEE ALSO 2B105.

 

 1. A process modified for one of the following:

 a. Pulsating CVD;

 b. Controlled nucleation thermal deposition (CNTD); or

 c. Plasma enhanced or plasma assisted CVD; and

 2. Having any of the following:

 a. Incorporating high vacuum (equal to or less than 0.01 Pa) rotating seals; or

 b. Incorporating in situ coating thickness control;

 

 b. Ion implantation production equipment having beam currents of 5 mA or more;

 

 c. Electron beam physical vapour deposition (EBPVD) production equipment incorporating power systems rated for over 80 kW and having any of the following:

 1. A liquid pool level “laser” control system which regulates precisely the ingots feed rate; or

 2. A computer controlled rate monitor operating on the principle of photoluminescence of the ionised atoms in the evaporant stream to control the deposition rate of a coating containing two or more elements;

 

 d. Plasma spraying production equipment having any of the following:

 1. Operating at reduced pressure controlled atmosphere (equal to or less than 10 kPa measured above and within 300 mm of the gun nozzle exit) in a vacuum chamber capable of evacuation down to 0.01 Pa prior to the spraying process; or

 2. Incorporating in situ coating thickness control;

 

 e. Sputter deposition production equipment capable of current densities of 0.1 mA/mm2 or higher at a deposition rate of 15 µm/h or more;

 

 f. Cathodic arc deposition production equipment incorporating a grid of electromagnets for steering control of the arc spot on the cathode;

 

 g. Ion plating production equipment allowing for the in situ measurement of any of the following:

 1. Coating thickness on the substrate and rate control; or

 2. Optical characteristics.

 

2B005 continued

 

 Note: 2B005 does not control chemical vapour deposition, cathodic arc, sputter deposition, ion plating or ion implantation equipment, specially designed for cutting or machining tools.

 

 

2B006 Dimensional inspection or measuring systems, equipment and “electronic assemblies”, as follows:

 

 a. Computer controlled or “numerically controlled” coordinate measuring machines (CMM), having a three dimensional (volumetric) maximum permissible error of indication (MPEE) at any point within the operating range of the machine (i.e., within the length of axes) equal to or less (better) than (1.7 + L/1,000) µm (L is the measured length in mm) tested according to ISO 103602 (2001);

 N.B.: SEE ALSO 2B206.

 

 b. Linear and angular displacement measuring instruments, as follows:

 1. Linear displacement measuring instruments having any of the following:

 Technical Note:

 For the purpose of 2B006.b.1. ‘linear displacement’ means the change of distance between the measuring probe and the measured object.

 

 a. Noncontact type measuring systems with a “resolution” equal to or less (better) than 0.2 µm within a measuring range up to 0.2 mm;

 

 b. Linear voltage differential transformer systems having all of the following:

 1. “Linearity” equal to or less (better) than 0.1% within a measuring range up to 5 mm; and

 2. Drift equal to or less (better) than 0.1% per day at a standard ambient test room temperature ±1 K;

 

 c. Measuring systems having all of the following:

 1. Containing a “laser”; and

 2. Maintaining, for at least 12 hours, at a temperature of 20±1 °C, all of the following:

 a. A “resolution” over their full scale of 0.1 µm or less (better); and

 b. Capable of achieving a “measurement uncertainty”, when compensated for the refractive index of air, equal to or less (better) than (0.2 + L/2,000) µm (L is the measured length in mm); or

 

 d. “Electronic assemblies” specially designed to provide feedback capability in systems specified in 2B006.b.1.c.;

 

2B006 b. continued

 

 Note: 2B006.b.1. does not control measuring interferometer systems, with an automatic control system that is designed to use no feedback techniques, containing a “laser” to measure slide movement errors of machinetools, dimensional inspection machines or similar equipment.

 

 2. Angular displacement measuring instruments having an “angular position deviation” equal to or less (better) than 0.00025°;

 Note: 2B006.b.2. does not control optical instruments, such as autocollimators, using collimated light (e.g., laser light) to detect angular displacement of a mirror.

 

 c. Equipment for measuring surface irregularities, by measuring optical scatter as a function of angle, with a sensitivity of 0.5 nm or less (better).

 

 Note: Machine tools, which can be used as measuring machines, are controlled if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.

 

 

2B007 “Robots” having any of the following characteristics and specially designed controllers and “endeffectors” therefor:

 N.B.: SEE ALSO 2B207.

 

 a. Capable in real time of full threedimensional image processing or full threedimensional ‘scene analysis’ to generate or modify “programs” or to generate or modify numerical program data;

 Technical Note:

 The ‘scene analysis’ limitation does not include approximation of the third dimension by viewing at a given angle, or limited grey scale interpretation for the perception of depth or texture for the approved tasks (2 1/2 D).

 

 b. Specially designed to comply with national safety standards applicable to potentially explosive munitions environments;

 Note: 2B007.b. does not control “robots” specially designed for paintspraying booths.

 

 c. Specially designed or rated as radiationhardened to withstand a total radiation dose greater than 5 x 103 Gy (silicon) without operational degradation; or

 Technical Note:

 The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation.

 

 d. Specially designed to operate at altitudes exceeding 30,000 m.

 

 

2B008 Assemblies or units, specially designed for machine tools, or dimensional inspection or measuring systems and equipment, as follows:

 

 a. Linear position feedback units (e.g., inductive type devices, graduated scales, infrared systems or “laser” systems) having an overall “accuracy” less (better) than (800 + (600 x L x 103)) nm (L equals the effective length in mm);

 N.B.: For “laser” systems see also Note to 2B006.b.1.c. and d.

 

 b. Rotary position feedback units (e.g., inductive type devices, graduated scales, infrared systems or “laser” systems) having an “accuracy” less (better) than 0.00025°;

 N.B.: For “laser” systems see also Note to 2B006.b.2.

 

 c. “Compound rotary tables” and “tilting spindles”, capable of upgrading, according to the manufacturer’s specifications, machine tools to or above the levels specified in 2B.

 

 

2B009 Spinforming machines and flowforming machines, which, according to the manufacturer’s technical specification, can be equipped with “numerical control” units or a computer control and having all of the following:

 N.B.: SEE ALSO 2B109 AND 2B209.

 

 a. Two or more controlled axes of which at least two can be coordinated simultaneously for “contouring control”; and

 b. A roller force more than 60 kN.

 

 Technical Note:

 For the purpose of 2B009, machines combining the function of spinforming and flowforming are regarded as flowforming machines.

 

 

2B104 “Isostatic presses”, not controlled in 2B004, having all of the following:

 N.B.: SEE ALSO 2B204.

 

 a. Maximum working pressure of 69 MPa or greater;

 b. Designed to achieve and maintain a controlled thermal environment of 873 K (600°C) or greater; and

 c. Possessing a chamber cavity with an inside diameter of 254 mm or greater.

 

 

2B105 Chemical vapour deposition (CVD) furnaces, not controlled in 2B005.a., designed or modified for the densification of carboncarbon composites.

 

 

2B109 Flowforming machines, not controlled in 2B009, and specially designed components as follows:

 N.B.: SEE ALSO 2B209.

 

 a. Flowforming machines having all of the following:

 1. According to the manufacturer’s technical specification, can be equipped with “numerical control” units or a computer control, even when not equipped with such units; and

 2. With more than two axes which can be coordinated simultaneously for “contouring control”.

 b. Specially designed components for flowforming machines specified in 2B009 or 2B109.a.

 

 Note: 2B109 does not control machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for systems specified in 9A005, 9A007.a. or 9A105.a.

 

 Technical Note:

 Machines combining the function of spinforming and flowforming are for the purpose of 2B109 regarded as flowforming machines.

 

 

2B116 Vibration test systems, equipment and components therefor, as follows:

 

 a. Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an

 acceleration equal to or greater than 10 g rms between 20 Hz and 2 kHz while imparting forces equal to or greater than 50 kN, measured ‘bare table’;

 

 b. Digital controllers, combined with specially designed vibration test software, with a realtime bandwidth greater than 5 kHz designed for use with vibration test systems specified in 2B116.a.;

 

 c. Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured ‘bare table’, and usable in vibration test systems specified in 2B116.a.;

 

 d. Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force of 50 kN, measured ‘bare table’, or greater, and usable in vibration systems specified in 2B116.a.

 

 Technical Note:

 In 2B116, ‘bare table’ means a flat table, or surface, with no fixture or fittings.

 

 

2B117 Equipment and process controls, not controlled in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.

2B119 Balancing machines and related equipment, as follows:

 N.B.: SEE ALSO 2B219.

 

 a. Balancing machines having all the following characteristics:

 1. Not capable of balancing rotors/assemblies having a mass greater than 3 kg;

 2. Capable of balancing rotors/assemblies at speeds greater than 12,500 rpm;

 3. Capable of correcting unbalance in two planes or more; and

 4. Capable of balancing to a residual specific unbalance of 0.2 g mm per kg of rotor mass;

 Note: 2B119.a. does not control balancing machines designed or modified for dental or other medical equipment.

 

 b. Indicator heads designed or modified for use with machines specified in 2B119.a.

 Technical Note:

 Indicator heads are sometimes known as balancing instrumentation.

 

 

2B120 Motion simulators or rate tables having all of the following characteristics:

 

 a. Two axes or more;

 

 b. Slip rings capable of transmitting electrical power and/or signal information; and

 

 c. Having any of the following characteristics:

 1. For any single axis having all of the following:

 a. Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; and

 b. A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0.6 degrees/s;

 2. Having a worstcase rate stability equal to or better (less) than plus or minus 0.05 % averaged over 10 degrees or more; or

 3. A positioning accuracy equal to or less (better) than 5 arc second.

 

 Note: 2B120 does not control rotary tables designed or modified for machine tools or for medical equipment.  For controls on machine tool rotary tables see 2B008.

 

 

2B121 Positioning tables (equipment capable of precise rotary positioning in any axes), not controlled in 2B120, having all the following characteristics:

 

 a. Two axes or more; and

 

 

 

 

2B121 continued

 

 b. A positioning accuracy equal to or less (better) than 5 arc second.

 

 Note: 2B121 does not control rotary tables designed or modified for machine tools or for medical equipment.  For controls on machine tool rotary tables see 2B008.

 

2B122 Centrifuges capable of imparting accelerations above 100 g and having slip rings capable of transmitting electrical power and signal information.

 

 

2B201 Machine tools and any combination thereof, not controlled in 2B001, as follows, for removing or cutting metals, ceramics or “composites”, which, according to the manufacturer’s technical specification, can be equipped with electronic devices for simultaneous “contouring control” in two or more axes:

 

 a. Machine tools for milling, having any of the following characteristics:

 1. Positioning accuracies with “all compensations available” equal to or less (better) than 6 µm according to ISO 230/2 (1988)[7] or national equivalents along any linear axis; or

 2. Two or more contouring rotary axes;

 Note: 2B201.a. does not control milling machines having the following characteristics:

  a. Xaxis travel greater than 2 m; and

  b. Overall positioning accuracy on the xaxis more (worse) than 30 µm.

 

 b. Machine tools for grinding, having any of the following characteristics:

 1. Positioning accuracies with “all compensations available” equal to or less (better) than 4 µm according to ISO 230/2 (1988)[8] or national equivalents along any linear axis; or

 2. Two or more contouring rotary axes.

 Note: 2B201.b. does not control the following grinding machines:

  a. Cylindrical external, internal, and externalinternal grinding machines having all of the following characteristics:

   1. Limited to a maximum workpiece capacity of 150 mm or length; and

   2. Axes limited to x, z and c;

 b. Jig grinders that do not have a zaxis or a waxis with an overall positioning accuracy less (better) than 4 µm according to ISO 230/2 (1988)[9] or national equivalents.

 

 

2B201 continued

 

 Note 1: 2B201 does not control special purpose machine tools limited to the manufacture of any of the following parts:

  a. Gears;

  b. Crankshafts or camshafts;

  c. Tools or cutters;

  d. Extruder worms.

 

 Note 2: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B001.a. or 2B201.a. or b.

 

 

2B204 “Isostatic presses”, other than those specified in 2B004 or 2B104, and related

 equipment, as follows:

 

 a. “Isostatic presses” having both of the following characteristics:

 1. Capable of achieving a maximum working pressure of 69 MPa or greater; and

 2. A chamber cavity with an inside diameter in excess of 152 mm;

 

 b. Dies, moulds and controls, specially designed for “isostatic presses” specified in 2B204.a.

 

Technical Note:

 In 2B204 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.

 

 

2B206 Dimensional inspection machines, instruments or systems, not controlled in 2B006, as follows:

 

 a. Computer controlled or numerically controlled dimensional inspection machines having both of the following characteristics:

 1. Two or more axes; and

 2. A onedimensional length “measurement uncertainty” equal to or less (better) than (1.25 + L/1000) µm tested with a probe of an “accuracy” of less (better) than 0.2 µm (L is the measured length in millimetres) (Ref.: VDI/VDE 2617 Parts 1 and 2);

 

 b. Systems for simultaneous linearangular inspection of hemishells, having both of the following characteristics:

 1. “Measurement uncertainty” along any linear axis equal to or less (better) than 3.5 µm per 5 mm; and

 2. “Angular position deviation” equal to or less than 0.02°.

 

2B206 continued

 

 Note 1: Machine tools that can be used as measuring machines are controlled if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.

 Note 2: A machine specified in 2B206 is controlled if it exceeds the control threshold anywhere within its operating range.

 

 Technical Notes:

 1. The probe used in determining the measurement uncertainty of a dimensional inspection system shall be described in VDI/VDE 2617 parts 2, 3 and 4.

 2. All parameters of measurement values in 2B206 represent plus/minus i.e., not total band.

 

 

2B207 “Robots”, “endeffectors” and control units, not controlled in 2B007, as follows:

 

 a. “Robots” or “endeffectors” specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives);

 

 b. Control units specially designed for any of the “robots” or “endeffectors” specified in 2B207.a.

 

 

2B209 Flow forming machines, spin forming machines capable of flow forming functions, not controlled in 2B009 or 2B109, and mandrels, as follows:

 

 a. Machines having both of the following characteristics:

 1. Three or more rollers (active or guiding); and

 2. Which, according to the manufacturer’s technical specification, can be equipped with “numerical control” units or a computer control;

 

 b. Rotorforming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm.

 

 Note: 2B209.a. includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process.

 

 

2B219 Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:

 

 a. Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:

 1. Swing or journal diameter greater than 75 mm;

 2. Mass capability of from 0.9 to 23 kg ; and

 3. Capable of balancing speed of revolution greater than 5,000 r.p.m.;

2B219 continued

 

 b. Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:

 1. Journal diameter greater than 75 mm;

 2. Mass capability of from 0.9 to 23 kg;

 3. Capable of balancing to a residual imbalance equal to or less than 0.01 kg x mm/kg per plane; and

 4. Belt drive type.

 

 

2B225 Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:

 

 a. A capability of penetrating 0.6 m or more of hot cell wall (throughthewall operation); or

 

 b. A capability of bridging over the top of a hot cell wall with a thickness of 0.6 m or more (overthewall operation).

 

 Technical Note:

 Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of ‘master/slave’ type or operated by joystick or keypad.

 

 

2B226 Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:

 N.B: SEE ALSO 3B.

 

 a. Furnaces having all of the following characteristics:

 1. Capable of operation above 1,123 K (850°C);

 2. Induction coils 600 mm or less in diameter; and

 3. Designed for power inputs of 5 kW or more;

 

 b. Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in 2B226.a.

 

 Note: 2B226.a. does not control furnaces designed for the processing of semiconductor wafers.

 


 

2B227 Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:

 

 a. Arc remelt and casting furnaces having both of the following characteristics:

 1. Consumable electrode capacities between 1,000 cm3 and 20,000 cm3; and

 2. Capable of operating with melting temperatures above 1,973 K (1,700oC);

 

 b. Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:

 1. A power of 50 kW or greater; and

 2. Capable of operating with melting temperatures above 1,473 K (1,200oC).

 

 c. Computer control and monitoring systems specially configured for any of the furnaces specified in 2B227.a. or b.

 

 

2B228 Rotor fabrication or assembly equipment, rotor straightening equipment,

 bellowsforming mandrels and dies, as follows:

 

 a. Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;

 Note: 2B228.a. includes precision mandrels, clamps, and shrink fit machines.

 

 b. Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;

 Technical Note:

 In 2B228.b. such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections.

 

 c. Bellowsforming mandrels and dies for producing singleconvolution bellows.

 Technical Note:

 In 2B228.c. the bellows have all of the following characteristics:

 1. Inside diameter between 75 mm and 400 mm;

 2. Length equal to or greater than 12.7 mm;

 3. Single convolution depth greater than 2 mm; and

 4. Made of highstrength aluminium alloys, maraging steel or high strength “fibrous or filamentary materials”.

 

 


2B230 “Pressure transducers” capable of measuring absolute pressures at any point in the range 0 to 13 kPa and having both of the following characteristics:

 

 a. Pressure sensing elements made of or protected by aluminium, aluminium alloy, nickel or nickel alloy with more than 60% nickel by weight; and

 

 b. Having either of the following characteristics:

 1. A full scale of less than 13 kPa and an ‘accuracy’ of better than + 1% of fullscale; or

 2. A full scale of 13 kPa or greater and an ‘accuracy’ of better than  + 130 Pa.

 

 Technical Note:

 For the purposes of 2B230, ‘accuracy’ includes nonlinearity, hysteresis and repeatability at ambient temperature.

 

 

2B231 Vacuum pumps having all of the following characteristics:

 

 a. Input throat size equal to or greater than 380 mm;

 b. Pumping speed equal to or greater than 15 m3/s; and

 c. Capable of producing an ultimate vacuum better than 13 mPa.

 Technical Notes:

 1. The pumping speed is determined at the measurement point with nitrogen gas or air.

 2. The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off.

 

 

2B232 Multistage light gas guns or other highvelocity gun systems (coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 2 km/s or greater.

 

2B350 Chemical manufacturing facilities, equipment and components, as follows:

 

 a. Reaction vessels or reactors, with or without agitators, with total internal (geometric) volume greater than 0.1 m3 (100 litres) and less than 20 m3 (20,000 litres), where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coating or glass lining);

 4. Nickel or alloys with more than 40% nickel by weight;

 5. Tantalum or tantalum alloys;

 6. Titanium or titanium alloys;

 7. Zirconium or zirconium alloys; or

 8. Niobium (columbium) or niobium alloys;

 

 

2B350 continued

 

 b. Agitators for use in reaction vessels or reactors specified in 2B350.a.; and impellers, blades or shafts designed for such agitators, where all surfaces of the agitator that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coatings or glass lining);

 4. Nickel or alloys with more than 40% nickel by weight;

 5. Tantalum or tantalum alloys;

 6. Titanium or titanium alloys;

 7. Zirconium or zirconium alloys; or

 8. Niobium (columbium) or niobium alloys;

 

 c. Storage tanks, containers or receivers with a total internal (geometric) volume greater than 0.1 m3 (100 litres) where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coatings or glass lining);

 4. Nickel or alloys with more than 40% nickel by weight;

 5. Tantalum or tantalum alloys;

 6. Titanium or titanium alloys;

 7. Zirconium or zirconium alloys; or

 8. Niobium (columbium) or niobium alloys;

 

 d. Heat exchangers or condensers with a heat transfer surface area greater than 0.15 m2, and less than 20 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coatings or glass lining);

 4. Graphite or ‘carbon graphite’;

 5. Nickel or alloys with more than 40% nickel by weight;

 6. Tantalum or tantalum alloys;

 7. Titanium or titanium alloys;

 8. Zirconium or zirconium alloys;

 9. Silicon carbide;

 10. Titanium carbide; or

 11. Niobium (columbium) or niobium alloys;

 

 e. Distillation or absorption columns of internal diameter greater than 0.1 m; and liquid distributors, vapour distributors or liquid collectors designed for such distillation or absorption columns, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

2B350 continued

 

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coatings or glass lining);

 4. Graphite or ‘carbon graphite’;

 5. Nickel or alloys with more than 40% nickel by weight;

 6. Tantalum or tantalum alloys;

 7. Titanium or titanium alloys;

 8. Zirconium or zirconium alloys; or

 9. Niobium (columbium) or niobium alloys;

 

 f. Remotely operated filling equipment in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight; or

2.         Nickel or alloys with more than 40% nickel by weight;

 

 g. Valves with nominal sizes greater than 10 mm and casings (valve bodies) or preformed casing liners designed for such valves, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coatings or glass lining);

 4. Nickel or alloys with more than 40% nickel by weight;

 5. Tantalum or tantalum alloys;

 6. Titanium or titanium alloys;

 7. Zirconium or zirconium alloys; or

 8. Niobium (columbium) or niobium alloys;

 

 h. Multiwalled piping incorporating a leak detection port, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Fluoropolymers;

 3. Glass (including vitrified or enamelled coatings or glass lining);

 4. Graphite or ‘carbon graphite’;

 5. Nickel or alloys with more than 40% nickel by weight;

 6. Tantalum or tantalum alloys;

 7. Titanium or titanium alloys;

 8. Zirconium or zirconium alloys; or

 9. Niobium (columbium) or niobium alloys;

 

2B350 continued

 

 i. Multipleseal and sealless pumps, with manufacturer’s specified maximum flowrate greater than 0.6 m3/hour, or vacuum pumps with manufacturer’s specified maximum flowrate greater than 5 m3/hour (under standard temperature (273 K (0oC)) and pressure (101.3 kPa) conditions); and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Ceramics;

 3. Ferrosilicon;

 4. Fluoropolymers;

 5. Glass (including vitrified or enamelled coatings or glass lining);

 6. Graphite or ‘carbon graphite’;

 7. Nickel or alloys with more than 40% nickel by weight;

 8. Tantalum or tantalum alloys;

 9. Titanium or titanium alloys;

 10. Zirconium or zirconium alloys; or

 11. Niobium (columbium) or niobium alloys;

 

 j. Incinerators designed to destroy chemicals specified in entry 1C350, having specially designed waste supply systems, special handling facilities and an average combustion chamber temperature greater than 1,273 K (1,000oC), in which all surfaces in the waste supply system that come into direct contact with the waste products are made from or lined with any of the following materials:

 1. Alloys with more than 25% nickel and 20% chromium by weight;

 2. Ceramics; or

 3. Nickel or alloys with more than 40% nickel by weight.

 

Technical Note:

‘Carbon graphite’ is a composition consisting of amorphous carbon and graphite, in which the graphite content is eight percent or more by weight.

 

 

2B351 Toxic gas monitoring systems, as follows; and dedicated detectors therefor:

 

 a. Designed for continuous operation and usable for the detection of chemical warfare agents or chemicals specified in 1C350, at concentrations of less than 0.3 mg/m3; or

 

 b. Designed for the detection of cholinesteraseinhibiting activity.

 

 


2B352 Equipment capable of use in handling biological materials, as follows:

 

 a. Complete biological containment facilities at P3, P4 containment level;

 Technical Note:

 P3 or P4 (BL3, BL4, L3, L4) containment levels are as specified in the WHO Laboratory Biosafety manual (3rd edition Geneva 2004).

 

 b. Fermenters capable of cultivation of pathogenic “microorganisms”, viruses or capable of toxin production, without the propagation of aerosols, and having a total capacity of 20 litres or more;

 Technical Note:

 Fermenters include bioreactors, chemostats and continuousflow systems.

 

 c. Centrifugal separators, capable of continuous separation without the propagation of aerosols, having all the following characteristics:

 1. Flow rate exceeding 100 litres per hour;

 2. Components of polished stainless steel or titanium;

 3. One or more sealing joints within the steam containment area; and

 4. Capable of insitu steam sterilisation in a closed state;

 Technical Note:

 Centrifugal separators include decanters.

 

 d. Cross (tangential) flow filtration equipment and components as follows:

  1. Cross (tangential) flow filtration equipment capable of separation of pathogenic microorganisms, viruses, toxins or cell cultures, without the propagation of aerosols, having both of the following characteristics:

 a. A total filtration area equal to or greater than1 m2; and

 b. Capable of being sterilised or disinfected insitu;

 Technical Note:

  In 2B352.d.1.b. sterilised denotes the elimination of all viable microbes from the equipment through the use of either physical (e.g. steam) or chemical agents. Disinfected denotes the destruction of potential microbial infectivity in the equipment through the use of chemical agents with a germicidal effect.  Disinfection and sterilisation are distinct from sanitisation, the latter referring to cleaning procedures designed to lower the microbial content of equipment without necessarily achieving elimination of all microbial infectivity or viability.

 

 2. Cross (tangential) flow filtration components (e.g. modules, elements, cassettes, cartridges, units or plates) with filtration area equal to or greater than 0.2 m2 for each component and designed for use in cross (tangential) flow filtration equipment specified in 2B352.d.;

 

  Note: 2B352.d. does not control reverse osmosis equipment, as specified by the manufacturer.

 

 e. Steam sterilisable freeze drying equipment with a condenser capacity exceeding 10 kg of ice in 24 hours and less than 1,000 kg of ice in 24 hours;

 

2B352 continued

 

 f. Protective and containment equipment, as follows:

 1. Protective full or half suits, or hoods dependent upon a tethered external air supply and operating under positive pressure;

 Note:  2B352.f.1. does not control suits designed to be worn with selfcontained breathing apparatus.

 2. Class III biological safety cabinets or isolators with similar performance standards;

 Note: In 2B352.f.2., isolators include flexible isolators, dry boxes, anaerobic chambers, glove boxes and laminar flow hoods (closed with vertical flow).

 

 g. Chambers designed for aerosol challenge testing with “microorganisms”, viruses or “toxins” and having a capacity of 1 m3 or greater.

 

 

2C Materials

 

 None.

 

 

2D Software

 

2D001 “Software”, other than that specified in 2D002, specially designed or modified for the “development”, “production” or “use” of equipment specified in 2A001 or 2B001 to 2B009.

 

 

2D002 “Software” for electronic devices, even when residing in an electronic device or

 system, enabling such devices or systems to function as a “numerical control” unit, capable of coordinating simultaneously more than four axes for “contouring control”.

 

 Note 1: 2D002 does not control “software” specially designed or modified for the operation of machine tools not controlled by Category 2.

 

 Note 2: 2D002 does not control “software” for items specified in 2B002.  See 2D001 for “software” for items specified in 2B002.

 

2D101 “Software” specially designed or modified for the “use” of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.

 N.B.: SEE ALSO 9D004.

 

 

2D201 “Software” specially designed for the “use” of equipment specified in 2B204, 2B206, 2B207, 2B209, 2B219 or 2B227.

 

 

2D202 “Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 2B201.

 

2E Technology

 

2E001 “Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 2A, 2B or 2D.

 

 

2E002 “Technology” according to the General Technology Note for the “production” of

 equipment specified in 2A or 2B.

 

 

2E003 Other “technology”, as follows:

 

 a. “Technology” for the “development” of interactive graphics as an integrated part in “numerical control” units for preparation or modification of part programs;

 

 b. “Technology” for metalworking manufacturing processes, as follows:

 

 1. “Technology” for the design of tools, dies or fixtures specially designed for any of the following processes:

 a. “Superplastic forming”;

 b. “Diffusion bonding”; or

 c. “Directacting hydraulic pressing”;

 

 2. Technical data consisting of process methods or parameters as listed below used to control:

 

 a. “Superplastic forming” of aluminium alloys, titanium alloys or “superalloys”:

 1. Surface preparation;

 2. Strain rate;

 3. Temperature;

 4. Pressure;

 

 b. “Diffusion bonding” of “superalloys” or titanium alloys:

 1. Surface preparation;

 2. Temperature;

 3. Pressure;

 

 c. “Directacting hydraulic pressing” of aluminium alloys or titanium alloys:

 1. Pressure;

 2. Cycle time;

 

 

 d. “Hot isostatic densification” of titanium alloys, aluminium alloys or “superalloys”:

 1. Temperature;

 2. Pressure;

 3. Cycle time;

2E003 continued

 

 c. “Technology” for the “development” or “production” of hydraulic stretchforming machines and dies therefor, for the manufacture of airframe structures;

 

 d. “Technology” for the “development” of generators of machine tool instructions (e.g., part programs) from design data residing inside “numerical control” units;

 

 e. “Technology” for the “development” of integration “software” for incorporation of expert systems for advanced decision support of shop floor operations into “numerical control” units;

 

 f. “Technology” for the application of inorganic overlay coatings or inorganic surface modification coatings (specified in column 3 of the following table) to nonelectronic substrates (specified in column 2 of the following table), by processes specified in column 1 of the following table and defined in the Technical Note.

 Note: The table and Technical Note appear after entry 2E301.

 

 

2E101 “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101.

 

 

2E201 “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 2A225, 2A226, 2B001, 2B006, 2B007.b., 2B007.c., 2B008, 2B009, 2B201, 2B204, 2B206, 2B207, 2B209, 2B225 to 2B232, 2D201 or 2D202.

 

 

2E301 “Technology” according to the General Technology Note for the “use” of goods

 specified in 2B350 to 2B352.


TABLE – DEPOSITION TECHNIQUES

 

 

1. Coating Process (1)[*] 2. Substrate 3. Resultant Coating

 

A. Chemical Vapour  “Superalloys”   Aluminides for internal

 Deposition  (CVD)    passages

 

   Ceramics (19) and Low  Silicides

   expansion glasses (14)  Carbides

     Dielectric layers (15)

     Diamond

     Diamondlike carbon (17)

 

   Carboncarbon,  Silicides

   Ceramic and  Carbides

   Metal “matrix”  Refractory metals

   “composites”  Mixtures thereof (4)

     Dielectric layers (15)

     Aluminides

     Alloyed aluminides (2)

     Boron nitride

 

   Cemented tungsten  Carbides

   carbide (16),  Tungsten

   Silicon carbide (18)  Mixtures thereof (4)

     Dielectric layers (15)

 

   Molybdenum and  Dielectric layers (15)

   Molybdenum alloys

 

   Beryllium and  Dielectric layers (15)

   Beryllium alloys  Diamond

     Diamondlike carbon (17)

 

   Sensor window  Dielectric layers (15)

   materials (9)  Diamond

     Diamondlike carbon (17)

 

___________________________________________________________________________

 


TABLE – DEPOSITION TECHNIQUES

 

1. Coating Process (1) 2. Substrate 3. Resultant Coating

 

B. ThermalEvaporation

 Physical Vapour

 Deposition (TEPVD)

 

B.1. Physical Vapour  “Superalloys”  Alloyed silicides

 Deposition (PVD):    Alloyed aluminides (2)

 ElectronBeam    McrAlX (5)

 (EBPVD)    Modified zirconia (12)

     Silicides

     Aluminides

     Mixtures thereof (4)

 

   Ceramics (19) and Low  Dielectric layers (15)

   expansion glasses (14)

 

   Corrosion resistant  McrAlX (5)

   steel (7)  Modified zirconia (12)

     Mixtures thereof (4)

 

   Carboncarbon,  Silicides

   Ceramic and  Carbides

   Metal “matrix”  Refractory metals

   “composites”  Mixtures thereof (4)

     Dielectric layers (15)

     Boron nitride

 

   Cemented tungsten  Carbides

   carbide (16),  Tungsten

   Silicon carbide (18)  Mixtures thereof (4)

     Dielectric layers (15)

 

   Molybdenum and  Dielectric layers (15)

   Molybdenum alloys

 

   Beryllium and  Dielectric layers (15)

   Beryllium alloys  Borides

     Beryllium

 

   Sensor window  Dielectric layers (15)

   materials (9)

 

   Titanium alloys (13)  Borides

     Nitrides

___________________________________________________________________________

 


TABLE – DEPOSITION TECHNIQUES

 

1. Coating Process (1) 2. Substrate 3. Resultant Coating

 

B.2. Ion assisted resistive  Ceramics (19) and Low  Dielectric layers (15)

 heating Physical Vapour  expansion glasses (14)  Diamondlike carbon (17)

 Deposition (PVD)

 (Ion Plating)

   Carboncarbon,  Dielectric layers (15)

   Ceramic and Metal  

   “matrix” “composites”  

 

   Cemented tungsten  Dielectric layers (15)

   carbide (16), 

   Silicon carbide 

 

   Molybdenum and 

   Molybdenum alloys  Dielectric layers (15)

 

   Beryllium and 

   Beryllium alloys  Dielectric layers (15)

 

   Sensor window  Dielectric layers (15)

   materials (9)  Diamondlike carbon (17)

___________________________________________________________________________

 

B.3. Physical Vapour  Ceramics (19) and Low  Silicides

 Deposition (PVD):  expansion glasses (14)  Dielectric layers (15)

 “Laser” Vaporization    Diamondlike carbon (17)

 

   Carboncarbon,  Dielectric layers (15)

   Ceramic and Metal

   “matrix” “composites”

 

   Cemented tungsten  Dielectric layers (15)

   carbide (16),

   Silicon carbide

 

   Molybdenum and  Dielectric layers (15)

   Molybdenum alloys

 

   Beryllium and  Dielectric layers (15)

   Beryllium alloys

 

   Sensor window  Dielectric layers (15)

   materials (9)  Diamondlike carbon

 

___________________________________________________________________________

 


TABLE – DEPOSITION TECHNIQUES

 

1. Coating Process (1) 2. Substrate 3. Resultant Coating

 

B.4. Physical Vapour  “Superalloys”  Alloyed silicides

 Deposition (PVD):    Alloyed aluminides (2)

 Cathodic Arc Discharge    McrAlX (5)

 

   Polymers (11) and  Borides

   Organic “matrix”  Carbides

   “composites”  Nitrides

     Diamondlike carbon (17)

___________________________________________________________________________

 

C. Pack cementation  Carboncarbon,  Silicides

 (see A above for  Ceramic and  Carbides

 outofpack  Metal “matrix”               Mixtures thereof (4)

 cementation) (10)  “composites”

 

   Titanium alloys (13)  Silicides

     Aluminides

     Alloyed aluminides (2)

  

 

   Refractory metals  Silicides

   and alloys (8)  Oxides

 

___________________________________________________________________________

 

D. Plasma spraying  “Superalloys”  McrAlX (5)

     Modified zirconia (12)

     Mixtures thereof (4)

     Abradable NickelGraphite

     Abradable materials

     containing NiCrAl

     Abradable AlSiPolyester

     Alloyed aluminides (2)

 

   Aluminium alloys (6)  McrAlX (5)

     Modified zirconia (12)

     Silicides

     Mixtures thereof (4)

 

   Refractory metals  Aluminides

   and alloys (8)  Silicides

     Carbides

 


TABLE – DEPOSITION TECHNIQUES

 

1. Coating Process (1) 2. Substrate 3. Resultant Coating

 

D. (continued)  Corrosion resistant  McrAlX (5)

   steel (7)  Modified zirconia (12)

     Mixtures thereof (4)

 

   Titanium alloys (13)  Carbides

     Aluminides

     Silicides

     Alloyed aluminides (2)

     Abradable NickelGraphite

     Abradable materials

     containing NiCrAl

     Abradable AlSiPolyester

 

___________________________________________________________________________

 

E. Slurry Deposition   Refractory metals  Fused silicides

   and alloys (8)  Fused aluminides

     except for resistance

     heating elements

 

   Carboncarbon,  Silicides

   Ceramic and  Carbides

   Metal “matrix”  Mixtures thereof (4)

   “composites”

___________________________________________________________________________

 

F. Sputter Deposition   “Superalloys”  Alloyed silicides

     Alloyed aluminides (2)

     Noble metal modified

     aluminides (3)

     McrAlX (5)

     Modified zirconia (12)

     Platinum

     Mixtures thereof (4)

 

   Ceramics and Low  Silicides

   expansion glasses (14)  Platinum

     Mixtures thereof (4)

     Dielectic layers (15)

     Diamondlike carbon (17)

 


TABLE – DEPOSITION TECHNIQUES

 

1. Coating Process (1) 2. Substrate 3. Resultant Coating

 

F. (continued)  Titanium alloys (13)  Borides

     Nitrides

     Oxides

     Silicides

     Aluminides

     Alloyed aluminides (2)

     Carbides

 

   Carboncarbon,  Silicides

   Ceramic and Metal  Carbides

   “matrix” “composites”  Refractory metals

     Mixtures thereof (4)

     Dielectric layers (15)

     Boron nitride

 

   Cemented tungsten  Carbides

   carbide (16),  Tungsten

   Silicon carbide (18)  Mixtures thereof (4)

     Dielectric layers (15)

     Boron nitride

 

   Molybdenum and

   Molybdenum alloys  Dielectric layers (15)

 

   Beryllium and  Borides

   Beryllium alloys  Dielectric layers (15)

     Beryllium

 

   Sensor window  Dielectric layers (15)

   materials (9)  Diamondlike carbon (17)

 

   Refractory metals  Aluminides

   and alloys (8)  Silicides

     Oxides

     Carbides

 

___________________________________________________________________________

 


TABLE – DEPOSITION TECHNIQUES

 

1. Coating Process (1) 2. Substrate 3. Resultant Coating

 

 

G. Ion Implantation   High temperature  Additions of

   bearing steels  Chromium

     Tantalum or

     Niobium (Columbium)

 

   Titanium alloys (13)  Borides

     Nitrides

 

   Beryllium and  Borides

   Beryllium alloys

 

   Cemented tungsten  Carbides

   carbide (16)  Nitrides

 

___________________________________________________________________________

 

 


TABLE – DEPOSITION TECHNIQUES – NOTES

 

1. The term ‘coating process’ includes coating repair and refurbishing as well as original coating.

 

2. The term ‘alloyed aluminide coating’ includes single or multiplestep coatings in which an element or elements are deposited prior to or during application of the aluminide coating, even if these elements are deposited by another coating process. It does not, however, include the multiple use of singlestep pack cementation processes to achieve alloyed aluminides.

 

3. The term ‘noble metal modified aluminide’ coating includes multiplestep coatings in which the noble metal or noble metals are laid down by some other coating process prior to application of the aluminide coating.

 

4. The term ‘mixtures thereof’ includes infiltrated material, graded compositions, codeposits and multilayer deposits and are obtained by one or more of the coating processes specified in the Table.

 

5. ‘McrAlX’ refers to a coating alloy where M equals cobalt, iron, nickel or combinations thereof and X equals hafnium, yttrium, silicon, tantalum in any amount or other intentional additions over 0.01 % by weight in various proportions and combinations, except:

a. CoCrAlY coatings which contain less than 22 % by weight of chromium, less than 7 % by weight of aluminium and less than 2 % by weight of yttrium;

b. CoCrAlY coatings which contain 22 to 24 % by weight of chromium, 10 to 12 % by weight of aluminium and 0.5 to 0.7 % by weight of yttrium; or

c. NiCrAlY coatings which contain 21 to 23 % by weight of chromium, 10 to 12 % by weight of aluminium and 0.9 to 1.1 % by weight of yttrium.

 

6. The term ‘aluminium alloys’ refers to alloys having an ultimate tensile strength of 190 Mpa or more measured at 293 K (20°C).

 

7. The term ‘corrosion resistant steel’ refers to AISI (American Iron and Steel Institute) 300 series or equivalent national standard steels.

 

8. ‘Refractory metals and alloys’ include the following metals and their alloys: niobium (columbium), molybdenum, tungsten and tantalum.

 

9. ‘Sensor window materials’, as follows: alumina, silicon, germanium, zinc sulphide, zinc selenide, gallium arsenide, diamond, gallium phosphide, sapphire and the following metal halides: sensor window materials of more than 40 mm diameter for zirconium fluoride and hafnium fluoride.

 

10. “Technology” for singlestep pack cementation of solid airfoils is not controlled by Category 2.

 

11. ‘Polymers’, as follows: polyimide, polyester, polysulphide, polycarbonates and polyurethanes.

 

12. ‘Modified zirconia’ refers to additions of other metal oxides (e.g., calcia, magnesia, yttria, hafnia, rare earth oxides) to zirconia in order to stabilise certain crystallographic phases and phase compositions.  Thermal barrier coatings made of zirconia, modified with calcia or magnesia by mixing or fusion, are not controlled.

 

13. ‘Titanium alloys’ refers only to aerospace alloys having an ultimate tensile strength of 900 Mpa or more measured at 293 K (20°C).

 

14. ‘Lowexpansion glasses’ refers to glasses which have a coefficient of thermal expansion of 1 x 107 K1 or less measured at 293 K (20°C).

 

15. ‘Dielectric layers’ are coatings constructed of multilayers of insulator materials in which the interference properties of a design composed of materials of various refractive indices are used to reflect, transmit or absorb various wavelength bands. Dielectric layers refers to more than four dielectric layers or dielectric/metal “composite” layers.

 

16. ‘Cemented tungsten carbide’ does not include cutting and forming tool materials consisting of tungsten carbide/(cobalt, nickel), titanium carbide/(cobalt, nickel), chromium carbide/nickelchromium and chromium carbide/nickel.

 

17. “Technology” specially designed to deposit diamondlike carbon on any of the following is not controlled:

 magnetic disk drives and heads, equipment for the manufacture of disposables, valves for faucets, acoustic diaphragms for speakers, engine parts for automobiles, cutting tools, punchingpressing dies, office automation equipment, microphones or medical devices or moulds, for casting or moulding of plastics, manufactured from alloys containing less than 5% beryllium.

 

18. ‘Silicon carbide’ does not include cutting and forming tool materials.

 

19. Ceramic substrates, as used in this entry, does not include ceramic materials containing 5% by weight, or greater, clay or cement content, either as separate constituents or in combination.

 

 


TABLE – DEPOSITION TECHNIQUES – TECHNICAL NOTE

 

Processes specified in Column 1 of the Table are defined as follows:

 

a. Chemical Vapour Deposition (CVD) is an overlay coating or surface modification coating process wherein a metal, alloy, “composite”, dielectric or ceramic is deposited upon a heated substrate.  Gaseous reactants are decomposed or combined in the vicinity of a substrate resulting in the deposition of the desired elemental, alloy or compound material on the substrate.  Energy for this decomposition or chemical reaction process may be provided by the heat of the substrate, a glow discharge plasma, or “laser” irradiation.

 

N.B.1 CVD includes the following processes: directed gas flow outofpack deposition, pulsating CVD, controlled nucleation thermal deposition (CNTD), plasma enhanced or plasma assisted CVD processes.

N.B.2 Pack denotes a substrate immersed in a powder mixture.

N.B.3 The gaseous reactants used in the outofpack process are produced using the same basic reactions and parameters as the pack cementation process, except that the substrate to be coated is not in contact with the powder mixture.

 

b. Thermal EvaporationPhysical Vapour Deposition (TEPVD) is an overlay coating process conducted in a vacuum with a pressure less than 0.1 Pa wherein a source of thermal energy is used to vaporize the coating material.  This process results in the condensation, or deposition, of the evaporated species onto appropriately positioned substrates.

 

 The addition of gases to the vacuum chamber during the coating process to synthesize compound coatings is an ordinary modification of the process.

 

 The use of ion or electron beams, or plasma, to activate or assist the coating’s deposition is also a common modification in this technique.  The use of monitors to provide inprocess measurement of optical characteristics and thickness of coatings can be a feature of these processes.

 

 Specific TEPVD processes are as follows:

 

1. Electron Beam PVD uses an electron beam to heat and evaporate the material which forms the coating;

2. Ion Assisted Resistive Heating PVD employs electrically resistive heating sources in combination with impinging ion beam(s) to produce a controlled and uniform flux of evaporated coating species;

3. “Laser” Vaporization uses either pulsed or continuous wave “laser” beams to vaporize the material which forms the coating;

4. Cathodic Arc Deposition employs a consumable cathode of the material which forms the coating and has an arc discharge established on the surface by a momentary contact of a ground trigger.  Controlled motion of arcing erodes the cathode surface creating a highly ionized plasma.  The anode can be either a cone attached to the periphery of the cathode, through an insulator, or the chamber.  Substrate biasing is used for non lineofsight deposition.

N.B. This definition does not include random cathodic arc deposition with nonbiased substrates.

5. Ion Plating is a special modification of a general TEPVD process in which a plasma or an ion source is used to ionize the species to be deposited, and a negative bias is applied to the substrate in order to facilitate the extraction of the species from the plasma.  The introduction of reactive species, evaporation of solids within the process chamber, and the use of monitors to provide inprocess measurement of optical characteristics and thicknesses of coatings are ordinary modifications of the process.

 

c. Pack Cementation is a surface modification coating or overlay coating process wherein a substrate is immersed in a powder mixture (a pack), that consists of:

1. The metallic powders that are to be deposited (usually aluminium, chromium, silicon or combinations thereof);

2. An activator (normally a halide salt); and

3. An inert powder, most frequently alumina.

 

 The substrate and powder mixture is contained within a retort which is heated to between 1,030 K (757°C) and 1,375 K (1,102°C) for sufficient time to deposit the coating.

 

d. Plasma Spraying is an overlay coating process wherein a gun (spray torch) which produces and controls a plasma accepts powder or wire coating materials, melts them and propels them towards a substrate, whereon an integrally bonded coating is formed.  Plasma spraying constitutes either low pressure plasma spraying or high velocity plasma spraying.

 

N.B.1 Low pressure means less than ambient atmospheric pressure.

N.B.2 High velocity refers to nozzleexit gas velocity exceeding 750 m/s calculated at 293 K (20°C) at 0.1 Mpa.

 

e. Slurry Deposition is a surface modification coating or overlay coating process wherein a metallic or ceramic powder with an organic binder is suspended in a liquid and is applied to a substrate by either spraying, dipping or painting, subsequent air or oven drying, and heat treatment to obtain the desired coating.

 

f. Sputter Deposition is an overlay coating process based on a momentum transfer phenomenon, wherein positive ions are accelerated by an electric field towards the surface of a target (coating material).  The kinetic energy of the impacting ions is sufficient to cause target surface atoms to be released and deposited on an appropriately positioned substrate.

 

N.B.1 The Table refers only to triode, magnetron or reactive sputter deposition which is used to increase adhesion of the coating and rate of deposition and to radio frequency (RF) augmented sputter deposition used to permit vaporisation of nonmetallic coating materials.

N.B.2 Lowenergy ion beams (less than 5 keV) can be used to activate the deposition.

 

g. Ion Implantation is a surface modification coating process in which the element to be alloyed is ionized, accelerated through a potential gradient and implanted into the surface region of the substrate.  This includes processes in which ion implantation is performed simultaneously with electron beam physical vapour deposition or sputter deposition.

 

CATEGORY 3 – ELECTRONICS

 

 

 

3A Systems, Equipment and Components

 

 Note 1: The control status of equipment and components described in 3A001 or 3A002, other than those described in 3A001.a.3. to 3A001.a.10. or 3A001.a.12., which are specially designed for or which have the same functional characteristics as other equipment is determined by the control status of the other equipment.

 

 Note 2: The control status of integrated circuits described in 3A001.a.3. to 3A001.a.9. or 3A001.a.12. which are unalterably programmed or designed for a specific function for another equipment is determined by the control status of the other equipment.

  N.B.: When the manufacturer or applicant cannot determine the control status of the other equipment, the control status of the integrated circuits is determined in 3A001.a.3. to 3A001.a.9. and 3A001.a.12.

   If the integrated circuit is a siliconbased “microcomputer microcircuit” or microcontroller microcircuit described in 3A001.a.3. having an operand (data) word length of 8 bit or less, the control status of the integrated circuit is determined in 3A001.a.3.

 

3A001 Electronic components and specially designed components therefor, as follows:

 

 a. General purpose integrated circuits, as follows:

 

 Note 1: The control status of wafers (finished or unfinished), in which the function has been determined, is to be evaluated against the parameters of 3A001.a.

 

 Note 2: Integrated circuits include the following types:

   “Monolithic integrated circuits”;

   “Hybrid integrated circuits”;

   “Multichip integrated circuits”;

“Film type integrated circuits”, including silicononsapphire integrated circuits;

   “Optical integrated circuits”.

 

 1. Integrated circuits designed or rated as radiation hardened to withstand any of the following:

 

 a. A total dose of 5 x 103  Gy (silicon) or higher;

 b. A dose rate upset of 5 x 106 Gy (silicon)/s or higher; or

3A001 a. 1. continued

 c. A fluence (integrated flux) of neutrons (1 MeV equivalent) of 5 x 1013 n/cm2 or higher on silicon, or its equivalent for other materials;

 

  Note: 3A001.a.1.c. does not apply to Metal Insulator Semiconductors (MIS).

 

 2. “Microprocessor microcircuits”, “microcomputer microcircuits”, microcontroller microcircuits, storage integrated circuits manufactured from a compound semiconductor, analoguetodigital converters, digitaltoanalogue converters, electrooptical or “optical integrated circuits” designed for “signal processing”, field programmable logic devices, custom integrated circuits for which either the function is unknown or the control status of the equipment in which the integrated circuit will be used is unknown, Fast Fourier Transform (FFT) processors, electrical erasable programmable readonly memories (EEPROMs), flash memories or static randomaccess memories (SRAMs), having any of the following:

 a. Rated for operation at an ambient temperature above 398 K (125°C);

 b. Rated for operation at an ambient temperature below 218 K (55°C); or

 c. Rated for operation over the entire ambient temperature range from 218 K (55°C) to 398 K (125°C);

 Note: 3A001.a.2. does not apply to integrated circuits for civil automobiles or railway train applications.

 

 3. “Microprocessor microcircuits”, “microcomputer microcircuits” and microcontroller microcircuits, manufactured from a compound semiconductor and operating at a clock frequency exceeding 40 MHz;

 Note: 3A001.a.3. includes digital signal processors, digital array processors and digital coprocessors.

 

 4. Storage integrated circuits manufactured from a compound semiconductor;

 

 5. Analoguetodigital and digitaltoanalogue converter integrated circuits, as follows:

 a. Analoguetodigital converters having any of the following:

 N.B. SEE ALSO 3A101

 1. A resolution of 8 bit or more, but less than 10 bit, with an output rate greater than 500 million words per second;

 2. A resolution of 10 bit or more, but less than 12 bit, with an output rate greater than 200 million words per second;

 3. A resolution of 12 bit with an output rate greater than 105 million words per second;

 4. A resolution of more than 12 bit, but equal to or less than 14 bit, with an output rate greater than 10 million words per second; or

3A001 a. 5. continued

 

 5. A resolution of more than 14 bit with an output rate greater than 2.5 million words per second;

 

 b. Digitaltoanalogue converters with a resolution of 12 bit or more and a “settling time” of less than 10 ns;

 Technical Notes:

1. A resolution of n bit corresponds to a quantisation of 2n levels.

2. The number of bits in the output word is equal to the resolution of the analoguetodigital converter.

3. The output rate is the maximum output rate of the converter, regardless of the architecture or oversampling.  Vendors may also refer to the output rate as sampling rate, conversion rate or throughput rate.  It is often specified in megahertz (MHz) or mega samples per second (MSPS).

4. For the purpose of measuring output rate, one output word per second is equivalent to one Hertz or one sample per second.

 

 6. Electrooptical and “optical integrated circuits”, designed for “signal processing” and having all of the following:

 a. One or more than one internal “laser” diode;

 b. One or more than one internal light detecting element; and

 c. Optical waveguides;

 

 7. ‘Field programmable logic devices’ having any of the following:

 a. An equivalent usable gate count of more than 30,000 (2 input gates);

 b. A typical “basic gate propagation delay time” of less than 0.1 ns; or

 c. A toggle frequency exceeding 133 MHz;

 

 Note: 3A001.a.7. includes:

    Simple Programmable Logic Devices (SPLDs)

    Complex Programmable Logic Devices (CPLDs)

    Field Programmable Gate Arrays (FPGAs)

    Field Programmable Logic Arrays (FPLAs)

    Field Programmable Interconnects (FPICs)

 

 Technical Note:

 ‘Field programmable logic devices’ are also known as field programmable gate or field programmable logic arrays.

 

 8. Deleted;

 

 9. Neural network integrated circuits;

 

 10. Custom integrated circuits for which the function is unknown, or the control status of the equipment in which the integrated circuits will be used is unknown to the manufacturer, having any of the following:

 a. More than 1,000 terminals;

3A001 a.10. continued

 

 b. A typical “basic gate propagation delay time” of less than 0.1 ns; or

 c. An operating frequency exceeding 3 GHz;

 

 11. Digital integrated circuits, other than those described in 3A001.a.3 to 3A001.a.10. and 3A001.a.12., based upon any compound semiconductor and having any of the following:

 a. An equivalent gate count of more than 3000 (2 input gates); or

 b. A toggle frequency exceeding 1.2 GHz;

 

 12. Fast Fourier Transform (FFT) processors having a rated execution time for an Npoint complex FFT of less than (N log2 N) /20,480 ms, where N is the number of points;

 Technical Note:

 When N is equal to 1,024 points, the formula in 3A001.a.12. gives an execution time of 500 µs.

 

 b. Microwave or millimetre wave components, as follows:

 

 1. Electronic vacuum tubes and cathodes, as follows:

 Note 1: 3A001.b.1. does not control tubes designed or rated for operation in any frequency band and having all of the following:

  a. Does not exceed 31.8 GHz; and

  b. Is “allocated by the ITU” for radiocommunications services, but not for radiodetermination.

 Note 2: 3A001.b.1. does not control non“spacequalified” tubes having all of the following:

  a. An average output power equal to or less than 50 W; and

  b. Designed or rated for operation in any frequency band and having all of the following:

   1.  Exceeds 31.8 GHz but does not exceed 43.5 GHz; and

   2.  Is “allocated by the ITU” for radiocommunications

        services, but not for radiodetermination.

 

 a. Travelling wave tubes, pulsed or continuous wave, as follows:

 1. Tubes operating at frequencies exceeding 31.8 GHz;

 2. Tubes having a cathode heater element with a turn on time to rated RF power of less than 3 seconds;

 3. Coupled cavity tubes, or derivatives thereof, with a “fractional bandwidth” of more than 7% or a peak power exceeding 2.5 kW;

 4. Helix tubes, or derivatives thereof, having any of the following:

 

 

3A001 b. 1. continued

 

 a. An “instantaneous bandwidth” of more than one octave, and average power (expressed in kW) times frequency (expressed in GHz) of more than 0.5;

 b. An “instantaneous bandwidth” of one octave or less, and average power (expressed in kW) times frequency (expressed in GHz) of more than 1; or

 c. Being “space qualified”;

 

 b. Crossedfield amplifier tubes with a gain of more than 17 dB;

 

 c. Impregnated cathodes designed for electronic tubes producing a continuous emission current density at rated operating conditions exceeding 5 A/cm2;

 

 2. Microwave “Monolithic Integrated Circuits” (MMIC) power amplifiers having any of the following:

 a. Rated for operation at frequencies exceeding 3.2 GHz up to and including 6 GHz and with an average output power greater than 4W (36 dBm) with a “fractional bandwidth” greater than 15%;

 b. Rated for operation at frequencies exceeding 6 GHz up to and including 16 GHz and with an average output power greater than 1W (30 dBm) with a “fractional bandwidth” greater than 10%;

 c. Rated for operation at frequencies exceeding 16 GHz up to and including 31.8 GHz and with an average output power greater than 0.8W (29 dBm) with a “fractional bandwidth” greater than 10%;

 d. Rated for operation at frequencies exceeding 31.8 GHz up to and including 37.5 GHz;

 e. Rated for operation at frequencies exceeding 37.5 GHz up to and including 43.5 GHz and with an average output power greater than 0.25W (24 dBm) with a “fractional bandwidth” greater than 10%; or

 f. Rated for operation at frequencies exceeding 43.5 GHz;

 Note 1: 3A001.b.2. does not control broadcast satellite equipment designed or rated to operate in the frequency range of 40.5 GHz to 42.5 GHz.

 Note 2: The control status of the MMIC whose rated operating frequency includes frequencies listed in more than one frequency range, as defined by 3A001.b.2.a. to 3A001.b.2.f., is determined by the lowest average output power control threshold.

 Note 3: Notes 1 and 2 in the chapeau to Category 3 mean that 3A001.b.2. does not control MMICs if they are specially designed for other applications, e.g., telecommunications, radar, automobiles.


3A001 b. continued

 

 3. Discrete microwave transistors having any of the following:

 a. Rated for operation at frequencies exceeding  3.2 GHz up to and including 6 GHz and having an average output power greater than 60W (47.8 dBm);

 b. Rated for operation at frequencies exceeding 6 GHz up to and including 31.8 GHz and having an average output power greater than 20W (43 dBm);

 c. Rated for operation at frequencies exceeding 31.8 GHz up to and including 37.5 GHz and having an average output power greater than 0.5W (27 dBm);

 

 d. Rated for operation at frequencies exceeding 37.5 GHz up to and including 43.5 GHz and having an average output power greater than 1W (30 dBm); or

 e. Rated for operation at frequencies exceeding 43.5 GHz;

  Note: The control status of a transistor whose rated operating frequency includes frequencies listed in more than one frequency range, as defined by 3A001.b.3.a. to 3A001.b.3.e., is determined by the lowest average output power control threshold.

 

 4. Microwave solid state amplifiers and microwave assemblies/modules containing microwave solid state amplifiers, having any of the following:

 a. Rated for operation at frequencies exceeding 3.2 GHz up to and including 6 GHz and with an average output power greater than 60W (47.8 dBm) with a “fractional bandwidth” greater than 15%;

 b. Rated for operation at frequencies exceeding 6 GHz up to and including 31.8 GHz and with an average output power greater than 15W (42 dBm) with a “fractional bandwidth” greater than 10%;

 c. Rated for operation at frequencies exceeding 31.8 GHz up to and including 37.5 GHz;

 d. Rated for operation at frequencies exceeding 37.5 GHz up to and including 43.5 GHz and with an average output power greater than 1W (30 dBm) with a fractional bandwidth” greater than 10%;

 e. Rated for operation at frequencies exceeding 43.5 GHz; or

 f. Rated for operation at frequencies above 3.2 GHz and having all of the following:

 1. An average output power (in watts), P, greater than 150 divided by the maximum operating frequency (in GHz) squared [P>150 W*GHz2/fGHz2];

 2. A “fractional bandwidth” of 5% or greater; and

 3. Any two sides perpendicular to one another with length d (in cm) equal to or less than 15 divided by the lowest operating frequency in GHz [d≤ 15cm*GHz/ fGHz];


3A001 b.4 continued

 

Technical Note:

3.2 GHz should be used as the lowest operating frequency (fGHz) in the formula in 3A001.b.4.f.3., for amplifiers that have a rated operating range extending downward to 3.2 GHz and below [d≤ 15cm*GHz/3.2 GHz].

 

 N.B.: MMIC power amplifiers should be evaluated against the criteria in 3A001.b.2.

 Note 1: 3A001.b.4. does not control broadcast satellite equipment designed or rated to operate in the frequency range of 40.5 to 42.5 GHz.

 Note 2: The control status of an item whose rated operating frequency includes frequencies listed in more than one frequency range, as defined by 3A001.b.4.a. to 3A001.b.4.e., is determined by the lowest average output power control threshold.

 

 5. Electronically or magnetically tunable bandpass or bandstop filters, having more than 5 tunable resonators capable of tuning across a 1.5:1 frequency band (fmax/fmin) in less than 10 µs and having any of the following:

 a. A bandpass bandwidth of more than 0.5% of centre frequency; or

 b. A bandstop bandwidth of less than 0.5% of centre frequency;

 

 6.  Deleted;

 

 7. Converters and harmonic mixers, designed to extend the frequency range of equipment described in 3A002.c., 3A002.d., 3A002.e. or 3A002.f. beyond the limits stated therein;

 

 8. Microwave power amplifiers containing tubes specified in 3A001.b.1. and having all of the following:

 a. Operating frequencies above 3 GHz;

 b. An average output power density exceeding 80 W/kg; and

 c. A volume of less than 400 cm3;

 Note: 3A001.b.8. does not control equipment designed or rated for operation in any frequency band which is “allocated by the ITU” for radiocommunications services, but not for radiodetermination.

 

9. Microwave power modules (MPM) consisting of, at least, a travelling wave tube, a microwave “monolithic integrated circuit” and an integrated electronic power conditioner therefor and having all of the following:

 a. A turnon time from off to fully operational in less than 10 seconds;

 

 

3A001 b.9 continued

 

 b. A volume less than the maximum rated power in Watts multiplied by 10 cm3/W; and

 c. An “instantaneous bandwidth” greater than 1 octave (fmax. > 2fmin.) and having any of the following:

 1. For frequencies equal to or less than 18 GHz, an RF output power greater than 100 W; or

2.         A frequency greater than 18 GHz;

Technical Notes:

1. To calculate the control volume in 3A001.b.9.b., the following example is provided: for a maximum rated power of 20 W, the volume would be: 20 W x 10 cm3/W = 200 cm3.

2. The turnon time in 3A001.b.9.a. refers to the time from fullyoff to fully operational; i.e., it includes the warmup time of the MPM.

 

 c. Acoustic wave devices as follows and specially designed components therefor:

 

 1. Surface acoustic wave and surface skimming (shallow bulk) acoustic wave devices (i.e., “signal processing” devices employing elastic waves in materials), having any of the following:

 a. A carrier frequency exceeding 6 GHz;

 b. A carrier frequency exceeding 1 GHz, but not exceeding 6 GHz, and having any of the following:

 1. A frequency sidelobe rejection exceeding 55 dB;

 2. A product of the maximum delay time and the bandwidth (time in µs and bandwidth in MHz) of more than 100;

 3. A bandwidth greater than 250 MHz; or

 4. A dispersive delay of more than 10 µs; or

 c. A carrier frequency of 1 GHz or less and having any of the following:

 1. A product of the maximum delay time and the bandwidth (time in µs and bandwidth in MHz) of more than 100;

 2. A dispersive delay of more than 10 µs; or

 3. A frequency sidelobe rejection exceeding 55 dB and a bandwidth greater than 100 MHz;

 

 2. Bulk (volume) acoustic wave devices (i.e., “signal processing” devices employing elastic waves) which permit the direct processing of signals at frequencies exceeding 2.5 GHz;

 

 3. Acousticoptic “signal processing” devices employing interaction between acoustic waves (bulk wave or surface wave) and light waves which permit the direct processing of signals or images, including spectral analysis, correlation or convolution;

 

 

 

 

3A001 continued

 

 d. Electronic devices and circuits containing components, manufactured from “superconductive” materials, specially designed for operation at temperatures below the “critical temperature” of at least one of the “superconductive” constituents and having any of the following:

 1. Current switching for digital circuits using “superconductive” gates with a product of delay time per gate (in seconds) and power dissipation per gate (in watts) of less than 1014 J; or

 2. Frequency selection at all frequencies using resonant circuits with Qvalues exceeding 10,000;

 

 e. High energy devices as follows:

 

 1. Cells as follows:

 

 a. Primary cells having an ‘energy density’ exceeding 550 Wh/kg at 20oC;

 b. Secondary cells having an ‘energy density’ exceeding 250 Wh/kg

 Technical Notes:

1. For the purpose of 3A001.e.1., ‘energy density’ (Wh/kg) is calculated from the nominal voltage multiplied by the nominal capacity in amperehours (Ah) divided by the mass in kilograms. If the nominal capacity is not stated, energy density is calculated from the nominal voltage squared then multiplied by the discharge duration in hours divided by the discharge load in ohms and the mass in kilograms.

2. For the purpose of 3A001.e.1., a ‘cell’ is defined as an electrochemical device, which has positive and negative electrodes, an electrolyte, and is a source of electrical energy.  It is the basic building block of a battery.

3. For the purpose of 3A001.e.1.a., a ‘primary cell’ is a ‘cell’ that is not designed to be charged by any other source.

4. For the purpose of 3A001.e.1.b., a ‘secondary cell’ is a ‘cell’ that is designed to be charged by an external electrical source.

 

 Note: 3A001.e.1. does not control batteries, including singlecell batteries.

 

 2. High energy storage capacitors as follows:

 N.B.:        SEE ALSO 3A201.a.

 a. Capacitors with a repetition rate of less than 10 Hz (single shot capacitors) and having all of the following:

 1. A voltage rating equal to or more than 5 kV;

 2. An energy density equal to or more than 250 J/kg; and

 3. A total energy equal to or more than 25 kJ;

 b. Capacitors with a repetition rate of 10 Hz or more (repetition rated capacitors) and having all of the following:

 1. A voltage rating equal to or more than 5 kV;

 2. An energy density equal to or more than 50 J/kg;

3A001 e. 2. continued

 

 3. A total energy equal to or more than 100 J; and

 4. A charge/discharge cycle life equal to or more than 10,000;

 

 3. “Superconductive” electromagnets and solenoids, specially designed to be fully charged or discharged in less than one second and having all of the following:

 N.B.:        SEE ALSO 3A201.b.

 Note: 3A001.e.3. does not control “superconductive” electromagnets or solenoids specially designed for Magnetic Resonance Imaging (MRI) medical equipment.

 a. Energy delivered during the discharge exceeding 10 kJ in the first second;

 b. Inner diameter of the current carrying windings of more than 250 mm; and

 c. Rated for a magnetic induction of more than 8 T or “overall current density” in the winding of more than 300 A/mm2;

 

4. Solar cells, cellinterconnectcoverglass (CIC) assemblies, solar panels, and solar arrays, which are “space qualified”, having a minimum average efficiency exceeding 20% at an operating temperature of 301 K (28°C) under simulated AM0 illumination with an irradiance of 1,367 watts per square metre (W/m2);

 

Technical Note:

 ‘AM0’, or ‘Air Mass Zero’, refers to the spectral irradiance of sun light in the earth’s outer atmosphere when the distance between the earth and sun is one astronomical unit (AU).

 

 f. Rotary input type shaft absolute position encoders having any of the following:

 1. A resolution of better than 1 part in 265,000 (18 bit resolution) of full scale; or

 2. An accuracy better than ± 2.5 seconds of arc;

 

g. Solidstate pulsed power switching thyristor devices and thyristor modules’, using either electrically, optically, or electron radiation controlled switch methods and having any of the following:

 1. A maximum turnon current rate of rise (di/dt) greater than 30,000 A/s and offstate voltage greater than 1,100 V; or

 2. A maximum turnon current rate of rise (di/dt) greater than 2,000 A/s and having all of the following:

 a. An offstate peak voltage equal to or greater than 3,000 V; and

 b. A peak (surge) current equal to or greater than 3,000 A.

 

 Note 1: 3A001.g. includes:

-          Silicon Controlled Rectifiers (SCRs)

-          Electrical Triggering Thyristors (ETTs)

-          Light Triggering Thyristors (LTTs)

3A002 g. continued

 

-          Integrated Gate Commutated Thyristors (IGCTs)

-          Gate Turnoff Thyristors (GTOs)

-          MOS Controlled Thyristors (MCTs)

-          Solidtrons

 

 Note 2: 3A001.g. does not control thyristor devices and thyristor modules incorporated into equipment designed for civil railway or “civil aircraft” applications.

 

 Technical Note:

 For the purposes of 3A001.g., a ‘thyristor module’ contains one or more thyristor devices.

 

 

3A002 General purpose electronic equipment and accessories therefor, as follows:

 

 a. Recording equipment as follows and specially designed test tape therefor:

 

 1. Analogue instrumentation magnetic tape recorders, including those permitting the recording of digital signals (e.g. using a high density digital recording (HDDR) module), having any of the following:

 a. A bandwidth exceeding 4 MHz per electronic channel or track;

 b. A bandwidth exceeding 2 MHz per electronic channel or track and having more than 42 tracks; or

 

 c. A time displacement (base) error, measured in accordance with applicable IRIG or EIA documents, of less than ± 0.1 µs;

 Note: Analogue magnetic tape recorders specially designed for civilian video purposes are not considered to be instrumentation tape recorders.

 

 2. Digital video magnetic tape recorders having a maximum digital interface transfer rate exceeding 360 Mbit/s;

 Note: 3A002.a.2. does not control digital video magnetic tape recorders specially designed for television recording using a signal format, which may include a compressed signal format, standardised or recommended by the ITU, the IEC, the SMPTE, the EBU, the ETSI or the IEEE  for civil television applications.

 

 3. Digital instrumentation magnetic tape data recorders employing helical scan techniques or fixed head techniques and having any of the following:

 a. A maximum digital interface transfer rate exceeding 175 Mbit/s; or

 b. Being “space qualified”;

 

 

3A002 a. continued

 

 Note: 3A002.a.3. does not control analogue magnetic tape recorders equipped with HDDR conversion electronics and configured to record only digital data.

 

 4. Equipment having a maximum digital interface transfer rate exceeding 175 Mbit/s and designed to convert digital video magnetic tape recorders for use as digital instrumentation data recorders;

 

 5. Waveform digitisers and transient recorders, having all of the following:

 a. Digitising rate equal to or more than  200 million samples per second and a resolution of 10 bit or more; and

 b. A continuous throughput of 2 Gbit/s or more;

 Technical Notes:

1. For those instruments with a parallel bus architecture, the continuous throughput rate is the highest word rate multiplied by the number of bits in a word.

2. ‘Continuous throughput’ is the fastest data rate the instrument can output to mass storage without the loss of any information whilst sustaining the sampling rate and analoguetodigital conversion.

 

 6. Digital instrumentation data recorders using magnetic disk storage technique and having all of the following:

 a. Digitising rate equal to or more than 100 million samples per second and a resolution of 8 bit or more; and

 b. A ‘continuous throughput’ of 1 Gbit/s or more;

 

 

 b. “Frequency synthesiser” “electronic assemblies” having a “frequency switching time” from one selected frequency to another of less than 1 ms;

 

Note: The control status of signal analysers, signal generators, network analysers, and microwave test receivers as standalone instruments is determined by 3A002.c., 3A002.d., 3A002.e., and 3A002.f., respectively.

 

 c. Radiofrequency “signal analysers” as follows:

 1. “Signal analysers” capable of analysing frequencies exceeding 31.8 GHz but not exceeding 37.5 GHz and having a 3 dB resolution bandwidth (RBW) exceeding 10 MHz;

 2. “Signal analysers” capable of analysing frequencies exceeding 43.5 GHz;

 3. “Dynamic signal analysers” having a “realtime bandwidth” exceeding 500 kHz;

 Note: 3A002.c.3. does not control those “dynamic signal analysers” using only constant percentage bandwidth filters (also known as octave or fractional octave filters).

 

3A002 continued

 

 d. Frequency synthesised signal generators producing output frequencies, the accuracy and short term and long term stability of which are controlled, derived from or disciplined by the internal master reference oscillator, and having any of the following:

 1. A maximum synthesised frequency exceeding31.8 GHz but not exceeding 43.5 GHz and rated to generate a pulse duration of less than 100 ns;

 2. A maximum synthesised frequency exceeding 43.5 GHz;

 3. A “frequency switching time” from one selected frequency to another as specified by any of the following:

 a. Less than 10 ns;

 b. Less than 100 µs for any frequency change exceeding 1.6 GHz within the synthesised frequency range exceeding 3.2 GHz but not exceeding 10.6 GHz;

 c. Less than 250 µs for any frequency change exceeding 550 MHz within the synthesised frequency range exceeding 10.6 GHz but not exceeding 31.8 GHz;

 d. Less than 500 µs for any frequency change exceeding 550 MHz within the synthesised frequency range exceeding 31.8 GHz but not exceeding 43.5 GHz; or

e. Less than 1 ms within the synthesised frequency range exceeding 43.5 GHz; or

 4. A single sideband (SSB) phase noise better than –(126 + 20 log10F – 20 log10f) in dBc/Hz, where F is the offset from the operating frequency in Hz and f is the operating frequency in MHz;

 

Note 1:  For the purpose of 3A002.d., frequency synthesised signal generators include arbitrary waveform and function generators.

 

 Note 2: 3A002.d. does not control equipment in which the output frequency is either produced by the addition or subtraction of two or more crystal oscillator frequencies, or by an addition or subtraction followed by a multiplication of the result.

 

Technical Notes:

1. Arbitrary waveform and function generators are normally specified by sample rate (e.g., Gsample/s), which is converted to the RF domain by the Nyquist factor of two. Thus, a 1 Gsample/s arbitrary waveform has a direct output capability of 500 MHz.  Or, when oversampling is used, the maximum direct output capability is proportionately lower.

2. For the purposes of 3A002.d.1., ‘pulse duration’ is defined as the time interval between the leading edge of the pulse achieving 90% of the peak and the trailing edge of the pulse achieving 10% of the peak.

 

 e. Network analysers with a maximum operating frequency exceeding 43.5 GHz;

 

 

3A002 continued

 

 f. Microwave test receivers having all of the following:

 1. A maximum operating frequency exceeding 43.5 GHz; and

 2. Being capable of measuring amplitude and phase simultaneously;

 

 g. Atomic frequency standards being any of the following:

 1. “Space qualified”;

 2. Nonrubidium and having a longterm stability less (better) than

  1 x 1011/month; or

  1. Non”space qualified” and having all of the following:

 a. Being a rubidium standard;

 b. Longterm stability less (better) than 1 x 1011/month; and

 c. Total power consumption of less than 1 W.

 

 

3A003 Spray cooling thermal management systems employing closed loop fluid handling and reconditioning equipment in a sealed enclosure where a dielectric fluid is sprayed onto electronic components using specially designed spray nozzles that are designed to maintain electronic components within their operating temperature range, and specially designed components therefor.

 

 

3A101 Electronic equipment, devices and components, not controlled in 3A001, as follows:

 

 a. Analoguetodigital converters, usable in “missiles”, designed to meet military specifications for ruggedized equipment;

 

 b. Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and systems containing those accelerators.

 Note: 3A101.b. above does not specify equipment specially designed for medical purposes.

 

 

3A102 Thermal batteries designed or modified for ‘missiles’.

 

Technical Notes:

1. In 3A102 thermal batteries are single use batteries that contain a solid nonconducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.

2. In 3A102 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 


 

3A201 Electronic components, not controlled in 3A001, as follows;

 

 a. Capacitors having either of the following sets of characteristics:

 1. a. Voltage rating greater than 1.4 kV;

 b. Energy storage greater than 10 J;

 c. Capacitance greater than 0.5 µF; and

 d. Series inductance less than 50 nH; or

 

 2. a. Voltage rating greater than 750 V;

 b. Capacitance greater than 0.25 µF; and

 c. Series inductance less than 10 nH;

 

 b. Superconducting solenoidal electromagnets having all of the following characteristics:

 1. Capable of creating magnetic fields greater than 2 T;

 2. A ratio of length to inner diameter greater than 2;

 3. Inner diameter greater than 300 mm; and

 4. Magnetic field uniform to better than 1% over the central 50% of the inner volume;

 Note: 3A201.b. does not control magnets specially designed for and exported ‘as parts of’ medical nuclear magnetic resonance (NMR) imaging systems.  The phrase ‘as part of’ does not necessarily mean physical part in the same shipment; separate shipments from different sources are allowed, provided the related export documents clearly specify that the shipments are dispatched ‘as part of’ the imaging systems.

 

 c. Flash Xray generators or pulsed electron accelerators having either of the following sets of characteristics:

 1. a. An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and

 b. With a ‘figure of merit’ (K) of 0.25 or greater; or

 2. a. An accelerator peak electron energy of 25 MeV or greater; and

 b. A ‘peak power’ greater than 50 MW.

 Note: 3A201.c. does not control accelerators that are component parts of devices designed for purposes other than electron beam or Xray radiation (electron microscopy, for example) nor those designed for medical purposes:

 

 Technical Notes:

 1. The ‘figure of merit’ K is defined as:

 

  K    =    1.7 x 103V2.65Q

 

  V is the peak electron energy in million electron volts.

 


3A201 c. continued

 

  If the accelerator beam pulse duration is less than or equal to 1 µs, then Q is the total accelerated charge in Coulombs.  If the accelerator beam pulse duration is greater than 1 µs, then Q is the maximum accelerated charge in 1 µs.

 

  Q equals the integral of i with respect to t, over the lesser of 1 µs or the time duration of the beam pulse (Q =  idt), where i is beam current in amperes and t is time in seconds.

 

 2. ‘Peak power’ = (peak potential in volts) x (peak beam current in amperes).

 

 3. In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 µs or the duration of the bunched beam packet resulting from one microwave modulator pulse.

 4. In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet.

 

 

3A225 Frequency changers or generators, not controlled in 0B001.b.13., having all of the following characteristics:

 

 a. Multiphase output capable of providing a power of 40 W or greater;

 b. Capable of operating in the frequency range between 600 and 2000 Hz;

 c. Total harmonic distortion better (less) than 10%; and

 d. Frequency control better (less) than 0.1%.

 

 Technical Note:

 Frequency changers in 3A225 are also known as converters or inverters.

 

 

3A226 Highpower direct current power supplies, not controlled in 0B001.j.6., having both of the following characteristics:

 

 a. Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and

 

 b. Current or voltage stability better than 0.1% over a time period of 8 hours.

 

 

3A227 Highvoltage direct current power supplies, not controlled in 0B001.j.5., having both of the following characteristics:

 

 a. Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and

 

 b. Current or voltage stability better than 0.1% over a time period of 8 hours.

 

3A228 Switching devices, as follows:

 

 a. Coldcathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:

 1. Containing three or more electrodes;

 2. Anode peak voltage rating of 2.5 kV or more;

 3. Anode peak current rating of 100 A or more; and

 4. Anode delay time of 10 µs or less;

 Note: 3A228 includes gas krytron tubes and vacuum sprytron tubes.

 

 b. Triggered sparkgaps having both of the following characteristics:

 1. An anode delay time of 15 µs or less; and

 2. Rated for a peak current of 500 A or more;

 

 c. Modules or assemblies with a fast switching function , other than those specified in 3A001.g., having all of the following characteristics:

 1. Anode peak voltage rating greater than 2 kV;

 2. Anode peak current rating of 500 A or more; and

 3. Turnon time of 1 µs or less.

 

 

3A229 Highcurrent pulse generators as follows:

 N.B.: SEE ALSO ML4.b.

 

 N.B. See 1A007.a. for explosive detonator firing sets.

 

 a. Deleted;

 

 b. Modular electrical pulse generators (pulsers) having all of the following characteristics:

 1. Designed for portable, mobile, or ruggedizeduse;

 2. Enclosed in a dusttight enclosure;

 3. Capable of delivering their energy in less than 15 µs;

 4. Having an output greater than 100 A;

 5. Having a ‘rise time’ of less than 10 µs into loads of less than 40 ohms;

 6. No dimension greater than 254 mm;

 7. Weight less than 25 kg; and

 8. Specified for use over an extended temperature range 223 K  (50oC) to 373 K (100oC) or specified as suitable for aerospace applications.

 

 Note: 3A229.b. includes xenon flashlamp drivers.

 

 Technical Note:

 In 3A229.b.5. ‘rise time’ is defined as the time interval from 10% to 90% current amplitude when driving a resistive load.

 


 

3A230 Highspeed pulse generators having both of the following characteristics:

 a. Output voltage greater than 6 V into a resistive load of less than 55 ohms, and

 b. ‘Pulse transition time’ less than 500 ps.

 Technical Note:

 In 3A230, ‘pulse transition time’ is defined as the time interval between 10% and 90% voltage amplitude.

 

 

3A231 Neutron generator systems, including tubes, having both of the following

 characteristics:

 a. Designed for operation without an external vacuum system; and

 b. Utilizing electrostatic acceleration to induce a tritiumdeuterium nuclear reaction.

 

 

3A232 Multipoint initiation systems, other than those specified in 1A007, as follows:

 N.B.: SEE ALSO ML4.b.

 

 N.B.: See 1A007.b. for detonators.

 

 a. Deleted;

 

 b. Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over greater than 5,000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2.5 µs.

 

 Note: 3A232 does not control detonators using only primary explosives, such as lead azide.

 

 

3A233 Mass spectrometers, not controlled in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:

 

 a. Inductively coupled plasma mass spectrometers (ICP/MS);

 b. Glow discharge mass spectrometers (GDMS);

 c. Thermal ionization mass spectrometers (TIMS);

 d. Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with materials resistant to UF6;

 e. Molecular beam mass spectrometers having either of the following characteristics:

 1. A source chamber constructed from, lined with or plated with stainless steel or molybdenum and equipped with a cold trap capable of cooling to 193 K (80oC) or less; or

 2. A source chamber constructed from, lined with or plated with materials resistant to UF6;

 f. Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.

 

3B Test, Inspection and Production Equipment

 

3B001 Equipment for the manufacturing of semiconductor devices or materials, as

 follows and specially designed components and accessories therefor:

 

 a. Equipment designed for epitaxial growth as follows:

 1. Equipment capable of producing a layer of any material other than silicon with a thickness uniform to less than ± 2.5% across a distance of 75 mm or more;

 2. Metal Organic Chemical Vapour Deposition (MOCVD) reactors specially designed for compound semiconductor crystal growth by the chemical reaction between materials specified in 3C003 or 3C004;

 3. Molecular beam epitaxial growth equipment using gas or solid sources;

 

 b. Equipment designed for ion implantation and having any of the following:

 1. A beam energy (accelerating voltage) exceeding 1MeV;

 2. Being specially designed and optimised to operate at a beam energy (accelerating voltage) of less than 2 keV;

 3. Direct write capability; or

 4. A beam energy of 65 keV or more and a beam current of 45 mA or more for high energy oxygen implant into a heated semiconductor material “substrate”;

 

 c. Anisotropic plasma dry etching equipment as follows:

 1. Equipment with cassettetocassette operation and loadlocks, and having any of the following:

 a. Designed or optimised to produce critical dimensions of 180 nm or less with ± 5% 3 sigma precision; or

 b. Designed for generating less than 0.04 particles/cm2 with a measurable particle size greater than 0.1 µm in diameter;

 2. Equipment specially designed for equipment specified in 3B001.e. and having any of the following:

 a. Designed or optimised to produce critical dimensions of 180 nm or less with ± 5% 3 sigma precision; or

 b. Designed for generating less than 0.04 particles/cm2 with a measurable particle size greater than 0.1 µm in diameter;

 

 d. Plasma enhanced Chemical Vapour Deposition (CVD) equipment as follows:

 1. Equipment with cassettetocassette operation and loadlocks, and designed according to the manufacturer’s specifications or optimised for use in the production of semiconductor devices with critical dimensions of 180 nm or less;

 

 2. Equipment specially designed for equipment specified in 3B001.e. designed according to the manufacturer’s specifications or optimised for use in the production of semiconductor devices with critical dimensions of 180 nm or less;

3B001 continued

 

 e. Automatic loading multichamber central wafer handling systems having all of the following:

 1. Interfaces for wafer input and output, to which more than two pieces of semiconductor processing equipment are to be connected; and

 2. Designed to form an integrated system in a vacuum environment for sequential multiple wafer processing;

 Note: 3B001.e. does not control automatic robotic wafer handling systems not designed to operate in a vacuum environment.

 

 f. Lithography equipment as follows:

 1. Align and expose step and repeat (direct step on wafer) or step and scan (scanner) equipment for wafer processing using photooptical or Xray methods and having any of the following:

 

 a. A light source wavelength shorter than 245 nm; or

 b. Capable of producing a pattern with a ‘minimum resolvable feature size’ of 180 nm or less;

 Technical Note:

 The ‘minimum resolvable feature size’ is calculated by the following formula:

 

 MRF = (an exposure light source wavelength in nm) x (K factor)

 numerical aperture

 

  where the K factor = 0.45

  MRF = minimum resolvable feature size

 

2. Imprint lithography equipment capable of producing features of 180 nm or less;

 Note: 3B001.f.2. includes:

a. Micro contact printing tools

b. Hot embossing tools

c. Nanoimprint lithography tools

d. Step and flash imprint lithography (SFIL) tools

 

 3. Equipment specially designed for mask making or semiconductor device processing using direct writing methods, having all of the following:

 a. Using deflected focussed electron beam, ion beam or “laser” beam; and

 b. Having any of the following:

 1. A spot size smaller than 0.2 µm;

 2. Being capable of producing a pattern with a feature size of less than 1 µm; or

 3. An overlay accuracy of better than ± 0.20 µm (3 sigma);

 

 g. Masks and reticles designed for integrated circuits specified in 3A001;

 

 h. Multilayer masks with a phase shift layer;

3B001 continued

 

 Note: 3B001.h. does not control multilayer masks with a phase shift layer designed for the fabrication of memory devices not controlled by 3A001.

 

i. Imprint lithography templates designed for integrated circuits specified in 3A001.

 

 

3B002 Test equipment specially designed for testing finished or unfinished semiconductor devices as follows and specially designed components and accessories therefor:

 

 a. For testing Sparameters of transistor devices at frequencies exceeding 31.8 GHz;

 

 b. Deleted;

 

 c. For testing microwave integrated circuits specified in 3A001.b.2.

 

 

3C Materials

 

3C001 Heteroepitaxial materials consisting of a “substrate” having stacked epitaxially grown multiple layers of any of the following:

 a. Silicon (Si);

 b. Germanium (Ge);

 c. Silicon carbide (SiC); or

 d. “III/V compounds” of gallium or indium.

 

 

3C002 Resist materials as follows and “substrates” coated with the following resists:

 

 a. Positive resists designed for semiconductor lithography specially adjusted (optimised) for use at wavelengths below 245 nm;

 

 b. All resists designed for use with electron beams or ion beams, with a sensitivity of 0.01 µcoulomb/mm2 or better;

 

 c. All resists designed for use with Xrays, with a sensitivity of 2.5 mJ/mm2 or better;

 

 d. All resists optimised for surface imaging technologies, including ‘silylated’ resists;

 Technical Note:

 ‘Silylation’ techniques are defined as processes incorporating oxidation of the resist surface to enhance performance for both wet and dry developing.

 

 

3C002 continued

 

 e. All resists designed or optimised for use with imprint lithography equipment specified by 3B001.f.2. that use either a thermal or photocurable process.

 

 

3C003 Organoinorganic compounds as follows:

 

 a. Organometallic compounds of aluminium, gallium or indium having a purity (metal basis) better than 99.999%;

 

 b. Organoarsenic, organoantimony and organophosphorus compounds having a purity (inorganic element basis) better than 99.999%.

 

 Note: 3C003 only controls compounds whose metallic, partly metallic or nonmetallic element is directly linked to carbon in the organic part of the molecule.

 

3C004 Hydrides of phosphorus, arsenic or antimony, having a purity better than 99.999%, even diluted in inert gases or hydrogen.

 

 Note: 3C004 does not control hydrides containing 20% molar or more of inert gases or hydrogen.

 

3C005 Silicon carbide (SiC), gallium nitride (GaN), aluminium nitride (AlN) or aluminium gallium nitride (AlGaN) “substrates”, or ingots, boules, or other preforms of those materials, having resistivities greater than 10,000 ohmcm at 20oC.

 

 

3C006 Substrates” specified in 3C005 with at least one epitaxial layer of silicon carbide, gallium nitride, aluminium nitride or aluminium gallium nitride.

 

 

3D Software

 

3D001 “Software” specially designed for the “development” or “production” of equipment               specified in 3A001.b. to  3A002.g. or 3B.

 

 

3D002 “Software” specially designed for the “use” of equipment specified in 3B001.a. to f. or 3B002.

 

 

3D003 Physicsbased simulation “software” specially designed for the “development” of

 lithographic, etching or deposition processes for translating masking patterns into specific topographical patterns in conductors, dielectrics or semiconductor materials.

 

 

3D003 continued

 

 Technical Note:

 ‘Physicsbased’ in 3D003 means using computations to determine a sequence of physical cause and effect events based on physical properties (e.g., temperature, pressure, diffusion constants and semiconductor materials properties).

 

 Note: Libraries, design attributes or associated data for the design of semiconductor devices or integrated circuits are considered as “technology”.

 

 

3D004 “Software” specially designed for the “development” of the equipment specified in 3A003.

 

 

3D101 “Software” specially designed or modified for the “use” of equipment specified in 3A101.b.

 

 

3E Technology

 

3E001 “Technology” according to the General Technology Note for the “development” or “production” of equipment or materials specified in 3A, 3B or 3C;

 

 Note 1: 3E001 does not control “technology” for the “production” of equipment or components controlled by 3A003.

 

 Note 2: 3E001 does not control “technology” for the “development” or “production” of integrated circuits specified in 3A001.a.3. to 3A001.a.12., having all of the following:

a. Using “technology” of 0.5 µm or more; and

b. Not incorporating ‘multilayer structures’.

 

Technical Note:

‘Multilayer structures’ do not include devices incorporating a maximum of three metal layers and three polysilicon layers.

 

 

3E002 “Technology” according to the General Technology Note, other than that specified in 3E001, for the “development” or “production” of a “microprocessor microcircuit”, “microcomputer microcircuit” or microcontroller microcircuit core, having an arithmetic logic unit with an access width of 32 bits or more and any of the following features or characteristics:

 

 a. A vector processor unit designed to perform more than two calculations on floatingpoint vectors (onedimensional arrays of 32bit or larger numbers) simultaneously;

 

3E002 continued

 

 Technical Note:

 A vector processor unit is a processor element with builtin instructions that perform multiple calculations on floatingpoint vectors (onedimensional arrays of 32bit or larger numbers) simultaneously, having at least one vector arithmetic logic unit.

 

 b. Designed to perform more than two 64bit or larger floatingpoint operation results per cycle; or

 

 c. Designed to perform more than four 16bit fixedpoint multiplyaccumulate results per cycle (e.g., digital manipulation of analogue information that has been previously converted into digital form, also known as digital signal processing).

 Note: 3E002.c. does not control “technology” for multimedia extensions.

 

 Note 1: 3E002 does not control “technology” for the “development” or “production” of microprocessor cores, having all of the following:

  a. Using “technology” at or above 0.130 µm; and

  b. Incorporating multilayer structures with five or fewer metal layers.

 

 Note 2: 3E002  includes “technology” for digital signal processors and digital array processors.

 

 

3E003 Other “technology” for the “development” or “production” of the following:

 

 a. Vacuum microelectronic devices;

 

 b. Heterostructure semiconductor devices such as high electron mobility transistors (HEMT), heterobipolar transistors (HBT), quantum well and super lattice devices;

 Note: 3E003.b. does not control “technology” for high electron mobility transistors (HEMT) operating at frequencies lower than 31.8 GHz and heterojunction bipolar transistors (HBT) operating at frequencies lower than 31.8 GHz.

 

 c. “Superconductive” electronic devices;

 

 d. Substrates of films of diamond for electronic components;

 

 e. Substrates of silicononinsulator (SOI) for integrated circuits in which the insulator is silicon dioxide;

 

 f. Substrates of silicon carbide for electronic components;

 

 g. Electronic vacuum tubes operating at frequencies of 31.8 GHz or higher.

 

 

3E101 “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 3A001.a.1. or 2., 3A101, 3A102 or 3D101.

 

 

3E102 “Technology” according to the General Technology Note for the “development” of “software” specified in 3D101.

 

 

3E201 “Technology” according to the General Technology Note for the “use” of equipment specified in 3A001.e.2., 3A001.e.3., 3A001.g., 3A201, 3A225 to 3A233.


 

CATEGORY 4 COMPUTERS

 

 

 Note 1: Computers, related equipment and “software” performing telecommunications or “local area network” functions must also be evaluated against the performance characteristics of Category 5 – Part 1 (Telecommunications).

 

 Note 2: Control units which directly interconnect the buses or channels of central processing units, “main storage” or disk controllers are not regarded as telecommunications equipment described in Category 5 – Part 1 (Telecommunications).

  N.B.: For the control status of “software” specially designed for packet switching, see 5D001.

 

 Note 3: Computers, related equipment and “software” performing cryptographic, cryptanalytic, certifiable multilevel security or certifiable user isolation functions, or which limit electromagnetic compatibility (EMC), must also be evaluated against the performance characteristics in Category 5 – Part 2 (“Information Security”).

 

 

4A Systems, Equipment and Components

 

4A001 Electronic computers and related equipment, having any of the following and “electronic assemblies” and specially designed components therefor:

 N.B.: SEE ALSO 4A101.

 

 a. Specially designed to have any of the following:

 1. Rated for operation at an ambient temperature below 228 K (45°C) or above 358 K (85°C); or

 Note: 4A001.a.1. does not control computers specially designed for civil automobile or railway  train applications.

 2. Radiation hardened to exceed any of the following specifications:

 a. Total Dose  5 x 103 Gy (silicon);

 b. Dose Rate Upset 5 x 106 Gy (silicon)/s; or

 c. Single Event Upset 1 x 107 Error/bit/day;

 

 b. Having characteristics or performing functions exceeding the limits in Category 5 – Part 2 (“Information Security”).

 Note: 4A001.b. does not control electronic computers and related equipment when accompanying their user for the user’s personal use.

 

 

4A003 “Digital computers”, “electronic assemblies”, and related equipment therefor, as

 follows and specially designed components therefor:

 

 Note 1: 4A003 includes the following:

   ‘Vector processors’;

   Array processors;

   Digital signal processors;

   Logic processors;

   Equipment designed for “image enhancement”;

   Equipment designed for “signal processing”.

 

 Note 2: The control status of the “digital computers” and related equipment described in 4A003 is determined by the control status of other equipment or systems provided:

 

  a. The “digital computers” or related equipment are essential for the operation of the other equipment or systems;

 

  b. The “digital computers” or related equipment are not a “principal element” of the other equipment or systems; and

 N.B. 1: The control status of “signal processing” or “image enhancement” equipment specially designed for other equipment with functions limited to those required for the other equipment is determined by the control status of the other equipment even if it exceeds the “principal element” criterion.

 N.B. 2: For the control status of “digital computers” or related equipment for telecommunications equipment, see Category 5 – Part 1 (Telecommunications).

 

  c. The “technology” for the “digital computers” and related equipment is determined by 4E.

 

 a. Designed or modified for “fault tolerance”;

 Note: For the purposes of 4A003.a., “digital computers” and related equipment are not considered to be designed or modified for “fault tolerance” if they utilise any of the following:

  1. Error detection or correction algorithms in “main storage”;

  2. The interconnection of two “digital computers” so that, if the active central processing unit fails, an idling but mirroring central processing unit can continue the system’s functioning;

  3. The interconnection of two central processing units by data channels or by using shared storage to permit one central processing unit to perform other work until the second central processing unit fails, at which time the first central processing unit takes over in order to continue the system’s functioning; or

4A003 a. continued

 

  4. The synchronisation of two central processing units by “software” so that one central processing unit recognises when the other central processing unit fails and recovers tasks from the failing unit.

 

 b. “Digital computers” having an “Adjusted Peak Performance” (“APP”) exceeding 0.75 Weighted TeraFLOPS (WT);

 

 c. “Electronic assemblies” specially designed or modified for enhancing performance by aggregation of processors so that the “APP” of the aggregation exceeds the limit specified in 4A003.b.;

 

 Note 1: 4A003.c. controls only “electronic assemblies” and programmable interconnections not exceeding the limit specified in 4A003.b. when shipped as unintegrated “electronic assemblies”.  It does not control “electronic assemblies” inherently limited by nature of their design for use as related equipment specified in 4A003.e.

 

 Note 2: 4A003.c. does not control “electronic assemblies” specially designed for a product or family of products whose maximum configuration does not exceed the limit specified in 4A003.b.

 

 d. Deleted;

 

 e. Equipment performing analoguetodigital conversions exceeding the limits specified in 3A001.a.5.;

 

 f. Deleted;

 

 g. Equipment specially designed to provide external interconnection of “digital computers” or associated equipment which allows communications at data rates exceeding 1.25 Gbyte/s.

 

 Note: 4A003.g. does not control internal interconnection equipment (e.g. backplanes, buses), passive interconnection equipment, “network access controllers” or “communications channel controllers”.

 

 

4A004 Computers as follows and specially designed related equipment, “electronic assemblies” and components therefor:

 

 a. “Systolic array computers”;

 b. “Neural computers”;

 c. “Optical computers”.

 

 

4A101 Analogue computers, “digital computers” or digital differential analysers, not controlled in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

4A102 “Hybrid computers” specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 Note: This control only applies when the equipment is supplied with “software” specified in 7D103 or 9D103.

 

 

4B Test, Inspection and Production Equipment

 

 None.

 

 

4C Materials

 

 None.

 

 

4D Software

 

 Note: The control status of “software” for the “development”, “production”, or “use” of equipment described in other Categories is dealt with in the appropriate Category. The control status of “software” for equipment described in this Category is dealt with herein.

 

 

4D001 “Software” as follows:

 

 a. “Software” specially designed or modified for the “development”, “production” or “use” of equipment or “software” specified in 4A001 to 4A004, or 4D.

 

 b. “Software”, other than that specified in 4D001.a., specially designed or modified for the “development” or “production” of equipment as follows:

 1. “Digital computers” having an “Adjusted Peak Performance” (“APP”) exceeding 0.04 Weighted TeraFLOPS (WT);

 2. “Electronic assemblies” specially designed or modified for enhancing performance by aggregation of processors so that the “APP” of the aggregation exceeds the limit in 4D001.b.1.;

 

 

4D002 “Software” specially designed or modified to support “technology” specified in 4E.

 

4D003 Specific “software” as follows:

 

 a. Operating system “software”, “software” development tools and compilers specially designed for “multidatastream processing” equipment, in “source code”;

 

 b. Deleted;

 

 c. “Software” having characteristics or performing functions exceeding the limits in Category 5 – Part 2 (“Information Security”);

 Note: 4D003.c. does not control “software” when accompanying its user for the user’s personal use.

 

 

4E Technology

 

4E001 a. “Technology” according to the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 4A or 4D.

 

 b. “Technology”, other than that specified in 4E001.a., specially designed or modified for the “development” or “production” of equipment as follows:

 1. “Digital computers” having an “Adjusted Peak Performance” (“APP”) exceeding 0.04 Weighted TeraFLOPS (WT);

 2. “Electronic assemblies” specially designed or modified for enhancing performance by aggregation of processors so that the “APP” of the aggregation exceeds the limit in 4E001.b.1.

 

 

 


TECHNICAL NOTE ON “ADJUSTED PEAK PERFORMANCE” (“APP”)

 

“APP” is an adjusted peak rate at which “digital computers” perform 64bit or larger floating point additions and multiplications.

 

“APP” is expressed in Weighted TeraFLOPS (WT), in units of 1012 adjusted floating point operations per second

 

n number of processors in the “digital computer”

i processor number (i,...n)

ti processor cycle time (ti = 1/Fi)

Fi processor frequency

Ri peak floating point calculating rate

Wi architecture adjustment factor

 

 

Outline of “APP” calculation method

 

1. For each processor i, determine the peak number of 64bit or larger floating point operations, FPOi, performed per cycle for each processor in the “digital computer”.

 

Note In determining FPO, include only 64bit or larger floating point additions and/or multiplications.  All floating point operations must be expressed in operations per processor cycle; operations requiring multiple cycles may be expressed in fractional results per cycle.  For processors not capable of performing calculations on floating point operands of 64bit or more, the effective calculating rate R is zero.

 

2. Calculate the floating point rate R for each processor   Ri = FPOi/ti.

 

3. Calculate “APP” as “APP” = W1 x R1 + W2 x R2 + … + Wn x Rn.

 

4. For vector processors, Wi = 0.9.  For nonvector processors, Wi = 0.3.

 

 

Note 1 For processors that perform compound operations in a cycle, such as addition and multiplication, each operation is counted.

 

Note 2 For a pipelined processor the effective calculating rate R is the faster of the pipelined rate, once the pipeline is full, or the nonpipelined rate.

 

Note 3 The calculating rate R of each contributing processor is to be calculated at its maximum value theoretically possible before the “APP” of the combination is derived.   Simultaneous operations are assumed to exist when the computer manufacturer claims concurrent, parallel, or simultaneous operation or execution in a manual or brochure for the computer.

 

 

 

TECHNICAL NOTE ON “ADJUSTED PEAK PERFORMANCE” (“APP”)

 

Note 4 Do not include processors that are limited to input/output and peripheral functions (e.g., disk drive, communication and video display) when calculating “APP”.

 

Note 5 “APP” values are not to be calculated for processor combinations (inter)connected by “Local Area Networks”, Wide Area Networks, I/O shared connections/devices, I/O controllers and any communication interconnection implemented by “software”.

 

Note 6 “APP” values must be calculated for:

1. Processor combinations containing processors specially designed to enhance performance by aggregation, operating simultaneously and sharing memory; or

2. Multiple memory/processor combinations operating simultaneously utilizing specially designed hardware.

 

Note 7 A vector processor is defined as a processor with builtin instructions that perform multiple calculations on floatingpoint vectors (onedimensional arrays of 64bit or larger numbers) simultaneously, having at least 2 vector functional units and at least 8 vector registers of at least 64 elements each.


 

CATEGORY 5 TELECOMMUNICATIONS AND “INFORMATION SECURITY”

 

 

 

Part 1 TELECOMMUNICATIONS

 

 

 Note 1: The control status of components, “lasers”, test and “production” equipment and “software” therefor which are specially designed for telecommunications equipment or systems is determined in Category 5 – Part 1.

 

 Note 2: “Digital computers”, related equipment or “software”, when essential for the operation and support of telecommunications equipment described in this Category, are regarded as specially designed components, provided they are the standard models customarily supplied by the manufacturer. This includes operation, administration, maintenance, engineering or billing computer systems.

 

 

5A1 Systems, Equipment and Components

 

5A001 Telecommunications systems, equipment, components and accessories as follows:

 

 a. Any type of telecommunications equipment having any of the following

  characteristics, functions or features:

 

 1. Specially designed to withstand transitory electronic effects or electromagnetic pulse effects, both arising from a nuclear explosion;

 2. Specially hardened to withstand gamma, neutron or ion radiation; or

 3. Specially designed to operate outside the temperature range from 218 K (55°C) to 397 K (124°C);

 Note: 5A001.a.3. applies only to electronic equipment.

 

 Note: 5A001.a.2. and 5A001.a.3. do not control equipment designed or modified for use on board satellites.

 

 b. Telecommunication systems and equipment, and specially designed components and accessories therefor, having any of the following characteristics, functions or features:

 

 1. Being underwater untethered communications systems having any of the following:

 a. An acoustic carrier frequency outside the range from 20 kHz to 60 kHz;

 b. Using an electromagnetic carrier frequency below 30 kHz;

 c. Using electronic beam steering techniques; or

5A001 b. continued

 

 d. Using “lasers” or lightemitting diodes (LEDs) with an output wavelength  greater than 400 nm and less than 700 nm, in a “local area network”;

 

 2. Being radio equipment operating in the 1.5 MHz to 87.5 MHz band and having all of the following:

 a. Automatically predicting and selecting frequencies and “total digital transfer rates” per channel to optimise the transmission; and

b. Incorporating a linear power amplifier configuration having a capability to support multiple signals simultaneously at an output power of 1 kW or more in the frequency range of 1.5 MHz or more but less than 30 MHz, or 250 W or more in the frequency range of 30 MHz or more but not exceeding 87.5 MHz, over an “instantaneous bandwidth” of one octave or more and with an output harmonic and distortion content of better than 80 dB;

 

 3. Being radio equipment employing “spread spectrum” techniques, including “frequency hopping” techniques, other than those specified in 5A001.b.4. and having any of the following:

 a. User programmable spreading codes; or

 b. A total transmitted bandwidth which is 100 or more times the bandwidth of any one information channel and in excess of 50 kHz;

 Note: 5A001.b.3.b. does not control radio equipment specially designed for use with civil cellular radiocommunications systems.

 

 Note: 5A001.b.3 does not control equipment designed to operate at an output power of 1 W or less.

 

 4. Being radio equipment employing ultrawideband modulation techniques, having user programmable channelising codes, scrambling codes or network identification codes and having any of the following:

 a. A bandwidth exceeding 500 MHz; or

 b. A “fractional bandwidth” of 20% or more;

 

 5. Being digitally controlled radio receivers having all of the following:

 a. More than 1,000 channels;

 b. A “frequency switching time” of less than 1 ms;

 c. Automatic searching or scanning of a part of the electromagnetic spectrum; and

 d. Identification of the received signals or the type of transmitter; or

 Note: 5A001.b.5. does not control radio equipment specially designed for use with civil cellular radiocommunications systems.

 

5A001 b. continued

 

 6. Employing functions of digital “signal processing” to provide ‘voice coding’ output at rates of less than 2,400 bit/s.

 Technical Notes:

1. For variable rate ‘voice coding’, 5A001.b.6. applies to the ‘voice coding’ output of continuous speech.

2. For the purposes of 5A001.b.6., ‘voice coding’ is defined as the technique to take samples of human voice and then convert these samples into a digital signal, taking into account specific characteristics of human speech.

 

 c. Optical fibre communication cables, optical fibres and accessories therefor, as follows:

 

 1. Optical fibres of more than 500 m in length, and specified by the manufacturer as being capable of withstanding a ‘proof test’ tensile stress of 2 x 109 N/m2 or more;

 Technical Note:

 ‘Proof Test’: online or offline production screen testing that dynamically applies a prescribed tensile stress over a 0.5 to 3 m length of fibre at a running rate of 2 to 5 m/s while passing between capstans approximately 150 mm in diameter.  The ambient temperature is a nominal 293 K (20oC) and relative humidity 40%.  Equivalent national standards may be used for executing the proof test.

 

 2. Optical fibre cables and accessories therefor, designed for underwater use;

 Note: 5A001.c.2. does not control  standard civil telecommunication cables and accessories.

 N.B. 1: For underwater umbilical cables, and connectors therefor, see 8A002.a.3.

 N.B. 2: For fibreoptic hull penetrators or connectors therefor, see 8A002.c.

 

 d. “Electronically steerable phased array antennae” operating above 31.8 GHz;

 Note: 5A001.d. does not control “electronically steerable phased array antennae” for landing systems with instruments meeting ICAO standards covering Microwave Landing Systems (MLS).

 

 e. Radio direction finding equipment operating at frequencies above 30 MHz and having all of the following, and specially designed components therefor:

 1. “Instantaneous bandwidth” of 10 MHz or more; and

 2. Capable of finding a Line Of Bearing (LOB) to noncooperating radio transmitters with a signal duration of less than 1 ms;

5A001 continued

 

 f. Jamming equipment specially designed or modified to intentionally and selectively interfere with, deny, inhibit, degrade or seduce mobile telecommunications services and having any of the following, and specially designed components therefor:

 1. Simulating the functions of Radio Access Network (RAN) equipment; or

 2. Detecting and exploiting specific characteristics of the mobile telecommunications protocol employed (e.g., GSM);

 

 N.B.: For GNSS jamming equipment see ML11.b.

 

g. Passive Coherent Location (PCL) systems or equipment specially designed for detecting and tracking moving objects by measuring reflections of ambient radio frequency emissions, supplied by nonradar transmitters.

 

 Technical Note:

 Nonradar transmitters may include commercial radio, television or cellular telecommunications base stations.

 

 Note: 5A001.g. does not control any of the following:

a. Radioastronomical equipment; or

b. Systems or equipment that require any radio transmission from the target.

 

 

5A101 Telemetry and telecontrol equipment, including ground equipment, designed or modified for ‘missiles’.

 

 Technical Note:

 In 5A101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 Note: 5A101 does not control:

  a. Equipment designed or modified for manned aircraft or satellites;

  b. Ground based equipment designed or modified for terrestrial or marine applications;

  c. Equipment designed for commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) GNSS services;

 


5B1 Test, Inspection and Production Equipment

 

5B001 Telecommunications test, inspection and production equipment, components and

 accessories, as follows:

 

 a. Equipment and specially designed components or accessories therefor, specially designed for the “development”, “production” or “use” of equipment, functions or features specified in 5A001, 5B001, 5D001 or 5E001;

 Note: 5B001.a. does not control optical fibre characterisation equipment.

 

 b. Equipment and specially designed components or accessories therefor, specially designed for the “development” of any of the following telecommunication transmission or switching equipment:

 

 1. Equipment employing digital techniques designed to operate at a “total digital transfer rate” exceeding 15 Gbit/s;

 Technical Note:

  For switching equipment the “total digital transfer rate” is measured at the highest speed port or line.

 

 2. Equipment employing a “laser” and having any of the following:

 a. A transmission wavelength exceeding 1750 nm;

 b. Performing “optical amplification”;

 c. Employing coherent optical transmission or coherent optical detection techniques (also called optical heterodyne or homodyne techniques); or

 d. Employing analogue techniques and having a bandwidth exceeding 2.5 GHz;

 Note: 5B001.b.2.d. does not control equipment specially designed for the “development” of commercial TV systems.

 

 3. Equipment employing “optical switching”;

 

 4. Radio equipment employing QuadratureAmplitudeModulation (QAM) techniques above level 256; or

 

 5. Equipment employing “common channel signalling” operating in nonassociated mode of operation.


5C1 Materials

 

 None

 

 

5D1 Software

 

5D001 “Software” as follows:

 

 a. “Software” specially designed or modified for the “development”, “production” or “use” of equipment, functions or features, specified in 5A001 or 5B001;

 

 b. “Software” specially designed or modified to support “technology” specified in 5E001;

 

 c. Specific “software” specially designed or modified to provide characteristics, functions or features of equipment specified in 5A001 or 5B001;

 

 d. “Software” specially designed or modified for the “development” of any of the following telecommunication transmission or switching equipment:

 

 1. Equipment employing digital techniques, including “Asynchronous Transfer Mode” (“ATM”), designed to operate at a “total digital transfer rate” exceeding 15 Gbit/s;

 Technical Note:

  For switching equipment the “total digital transfer rate” is measured at the highest speed port or line.

 

 2. Equipment employing a “laser” and having any of the following:

 a. A transmission wavelength exceeding 1,750 nm; or

 b. Employing analogue techniques and having a bandwidth exceeding 2.5 GHz;

 Note: 5D001.d.2.b. does not control “software” specially designed or modified for the “development” of commercial TV systems.

 

 3. Equipment employing “optical switching”; or

 

 4. Radio equipment employing QuadratureAmplitudeModulation (QAM) techniques above level 256.

 

 

5D101 “Software” specially designed or modified for the “use” of equipment specified in               5A101.

 

 


5E1 Technology

 

5E001 “Technology” as follows:

 

 a. “Technology” according to the General Technology Note for the

  “development”, “production” or “use” (excluding operation) of equipment, functions or features or “software”, specified in 5A001, 5B001 or 5D001;

 

 b. Specific “technology” as follows:

 

 1. “Required” “technology” for the “development” or “production” of telecommunications equipment specially designed to be used on board satellites;

 

 2. “Technology” for the “development” or “use” of “laser” communication techniques with the capability of automatically acquiring and tracking signals and maintaining communications through exoatmosphere or subsurface (water) media;

 

 3. “Technology” for the “development” of digital cellular radio base station receiving equipment whose reception capabilities that allow multiband, multichannel, multimode, multicoding algorithm or multiprotocol operation can be modified by changes in “software”;

 

 4. “Technology” for the “development” of “spread spectrum” techniques, including “frequency hopping” techniques;

 

 c. “Technology” according to the General Technology Note for the “development” or “production” of any of the following:

 

 1. Equipment employing digital techniques designed to operate at a “total digital transfer rate” exceeding 15 Gbit/s;

 Technical Note:

  For switching equipment the “total digital transfer rate” is measured at the highest speed port or line.

 

 2. Equipment employing a “laser” and having any of the following:

 a. A transmission wavelength exceeding 1,750 nm;

 b. Performing “optical amplification” using PraseodymiumDoped Fluoride Fibre Amplifiers (PDFFA);

 c. Employing coherent optical transmission or coherent optical detection techniques (also called optical heterodyne or homodyne techniques);

 d. Employing wavelength division multiplexing techniques exceeding 8 optical carriers in a single optical window; or

 e. Employing analogue techniques and having a bandwidth exceeding 2.5 GHz;

 Note: 5E001.c.2.e. does not control “technology” for the “development” or “production” of commercial TV systems.

5B001 c. continued

 

 3. Equipment employing “optical switching”;

 

 4. Radio equipment having any of the following:

 a. QuadratureAmplitudeModulation (QAM) techniques above level 256;

 b. Operating at input or output frequencies exceeding31.8 GHz; or

 Note: 5E001.c.4.b. does not control “technology” for the “development” or “production” of equipment designed or modified for operation in any frequency band which is “allocated by the ITU” for radiocommunications services, but not for radiodetermination.

c. Operating in the 1.5 MHz to 87.5 MHz band and incorporating adaptive techniques providing more than 15 dB suppression of an interfering signal; or

 

 5. Equipment employing “common channel signalling” operating in nonassociated mode of operation.

 

 

5E101 “Technology” according to the General Technology Note for the “development”,

 “production” or “use” of equipment specified in 5A101.

 

 


Part 2 “INFORMATION SECURITY”

 

 Note 1: The control status of “information security” equipment, “software”, systems, application specific “electronic assemblies”, modules, integrated circuits, components or functions is determined in Category 5 – Part 2 even if they are components or “electronic assemblies” of other equipment.

N.B.: Category 5 – Part 2 does not control equipment and software specially designed for medical enduse incorporating an item specified in Category 5 – Part 2.

 

 Note 2: Category 5 – Part 2 does not control products when accompanying their user for the user’s personal use.

 

 Note 3: Cryptography Note

 

  5A002 and 5D002 do not control goods that meet all of the following:

 

  a. Generally available to the public by being sold, without restriction, from stock at retail selling points by means of any of the following:

  1. Overthecounter transactions;

  2. Mail order transactions;

  3. Electronic transactions; or

  4. Telephone call transactions;

 

  b. The cryptographic functionality cannot easily be changed by the user;

 

  c. Designed for installation by the user without further substantial support by the supplier; and

 

  d. When necessary, details of the goods are accessible and will be provided, upon request, to the competent authorities of the Member State in which the exporter is established in order to ascertain compliance with conditions described in paragraphs a. to c. above.

 

 Technical Note:

 In Category 5 – Part 2, parity bits are not included in the key length.

 

 


5A2 Systems, Equipment and Components

 

5A002 “Information security” systems, equipment and components therefor, as follows:

 

 a. Systems, equipment, application specific “electronic assemblies”, modules and integrated circuits for “information security”, as follows, and other specially designed components therefor:

 N.B.: For the control of Global Navigation Satellite Systems (GNSS) receiving equipment containing or employing decryption (i.e., GPS or GLONASS), see 7A005.

 

 1. Designed or modified to use “cryptography” employing digital techniques performing any cryptographic function other than authentication or digital signature and having any of the following:

 

 Technical Notes:

1. Authentication and digital signature functions include their associated key management function.

2. Authentication includes all aspects of access control where there is no encryption of files or text except as directly related to the protection of passwords, Personal Identification Numbers (PINs) or similar data to prevent unauthorised access.

3. “Cryptography” does not include “fixed” data compression or coding techniques.

 

 Note: 5A002.a.1. includes equipment designed or modified to use “cryptography” employing analogue principles when implemented with digital techniques.

 

 a. A “symmetric algorithm” employing a key length in excess of 56 bits; or

 

 b. An “asymmetric algorithm” where the security of the algorithm is based on any of the following:

 1. Factorisation of integers in excess of 512 bits (e.g., RSA);

 2. Computation of discrete logarithms in a multiplicative group of a finite field of size greater than 512 bits (e.g., DiffieHellman over Z/pZ); or

 3. Discrete logarithms in a group other than mentioned in 5A002.a.1.b.2. in excess of 112 bits (e.g., DiffieHellman over an elliptic curve);

 

 2. Designed or modified to perform cryptanalytic functions;

 

 3. Deleted;

 

 4. Specially designed or modified to reduce the compromising emanations of informationbearing signals beyond what is necessary for health, safety or electromagnetic interference standards;

 

 

5A002 continued

 

 5. Designed or modified to use cryptographic techniques to generate the spreading code for “spread spectrum” systems, other than those specified in 5A002.a.6., including the hopping code for “frequency hopping” systems;

 

 6. Designed or modified to use cryptographic techniques to generate channelising codes, scrambling codes or network identification codes, for systems using ultrawideband modulation techniques and having any of the following:

 

a. A bandwidth exceeding 500 MHz; or

 

b. A “fractional bandwidth” of 20% or more;

 

 7. Deleted;

 

 8. Communications cable systems designed or modified using mechanical, electrical or electronic means to detect surreptitious intrusion;

 

 9. Designed or modified to use “quantum cryptography”.

 Technical Note:

 “Quantum cryptography” is also known as Quantum Key Distribution (QKD).

 

 Note: 5A002 does not control any of the following:

 

  a. “Personalised smart cards” having any of the following:

  1. Where the cryptographic capability is restricted for use in equipment or systems excluded from control under entries b. to g. of this Note; or

  2. For general publicuse applications where the cryptographic capability is not useraccessible and it is specially designed and limited to allow protection of personal data stored within;

N.B.: If a “personalised smart card” has multiple functions, the control status of each function is assessed individually.

 

  b. Receiving equipment for radio broadcast, pay television or similar restricted audience broadcast of the consumer type, without digital encryption except that exclusively used for sending the billing or programmerelated information back to the broadcast providers;

 

  c. Equipment where the cryptographic capability is not useraccessible and which is specially designed and limited to allow any of the following:

  1. Execution of copyprotected “software”;

5A002 c. continued

 

  2. Access to any of the following:

a. Copyprotected contents stored on readonly media; or

b. Information stored in encrypted form on media (e.g., in connection with the protection of intellectual property rights) when the media is offered for sale in identical sets to the public;

  3. Copying control of copyright protected audio/video data; or

  4. Encryption and/or decryption for protection of libraries, design attributes, or associated data for the design of semiconductor devices or integrated circuits;

 

  d. Cryptographic equipment specially designed and limited for banking use or ‘money transactions’;

  Technical Note:

   ‘Money transactions’ in 5A002 Note d. includes the collection and settlement of fares or credit functions.

 

  e. Portable or mobile radiotelephones for civil use (e.g., for use with commercial civil cellular radio communication systems) that are not capable of transmitting encrypted data directly to another radiotelephone or equipment (other than Radio Access Network (RAN) equipment), nor of passing encrypted data through RAN equipment (e.g., Radio Network Controller (RNC) or Base Station Controller (BSC));

 

  f. Cordless telephone equipment not capable of endtoend encryption where the maximum effective range of unboosted cordless operation (i.e. a single, unrelayed hop between terminal and home base station) is less than 400 metres according to the manufacturer’s specifications; or

 

  g. Portable or mobile radiotelephones and similar client wireless devices for civil use, that implement only published or commercial cryptographic standards (except for antipiracy functions, which may be nonpublished) and also meet the provisions of paragraphs b. to d. of the Cryptography Note (Note 3 in Category 5 Part 2), that have been customised for a specific civil industry application with features that do not affect the cryptographic functionality of these original noncustomised devices.

 

 

5B2 Test, Inspection and Production Equipment

 

5B002 “Information security” test, inspection and “production” equipment, as follows:

 

 a. Equipment specially designed for “development” or “production”, as follows:

 

 

5B002 a. continued

 

 1. “Development” of equipment or functions, specified in 5A002, 5B002, 5D002 or 5E002 including measuring or test equipment;

 

 2. “Production” of equipment or functions, specified in 5A002, 5B002, 5D002 or 5E002, including measuring, test, repair or “production” equipment;

 

 b. Measuring equipment specially designed to evaluate and validate the “information security” functions specified in 5A002 or 5D002.

 

 

5C2 Materials

 

 None.

 

 

5D2 Software

 

5D002 “Software” as follows:

 

 a. “Software” specially designed or modified for the “development”, “production” or “use” of equipment or “software”, specified in 5A002, 5B002 or 5D002;

 

 b. “Software” specially designed or modified to support “technology” specified in 5E002;

 

 c. Specific “software”, as follows:

 1. “Software” having the characteristics, or performing or simulating the functions of the equipment, specified in 5A002 or 5B002;

 2. “Software” to certify “software” specified in 5D002.c.1.

 

 Note: 5D002 does not control “software” as follows:

  a. “Software” required for the “use” of equipment excluded from control by the Note to 5A002;

  b. “Software” providing any of the functions of equipment excluded from control by the Note to 5A002.

 

 

5E2 Technology

 

5E002 “Technology” according to the General Technology Note for the “development”,

 “production” or “use” of equipment or “software”, specified in 5A002, 5B002 or 5D002.

 

CATEGORY 6 SENSORS AND LASERS

 

 

 

6A Systems, Equipment and Components

 

6A001 Acoustic systems, equipment and components, as follows:

 

 a. Marine acoustic systems, equipment and specially designed components therefor, as follows:

 

 1. Active (transmitting or transmittingandreceiving) systems, equipment and specially designed components therefor, as follows:

 

 Note: 6A001.a.1. does not control equipment as follows:

  a. Depth sounders operating vertically below the apparatus, not including a scanning function exceeding ± 20°, and limited to measuring the depth of water, the distance of submerged or buried objects or fish finding;

  b. Acoustic beacons, as follows:

 1. Acoustic emergency beacons;

 2. Pingers specially designed for relocating or returning to an underwater position.

 

 a. Wideswath bathymetric survey systems designed for sea bed topographic mapping and having all of the following:

 1. Designed to take measurements at an angle exceeding 20° from the vertical;

 2. Designed to measure depths exceeding 600 m below the water surface; and

 3. Designed to provide any of the following:

 a. Incorporation of multiple beams any of which is less than 1.9°; or

 b. Data accuracies of better than 0.3% of water depth across the swath averaged over the individual measurements within the swath;

 

 b. Object detection or location systems having any of the following:

 1. A transmitting frequency below 10 kHz;

 2. Sound pressure level exceeding 224 dB (reference 1 µPa at 1 m) for equipment with an operating frequency in the band from 10 kHz to 24 kHz inclusive;

 3. Sound pressure level exceeding 235 dB (reference 1 µPa at 1 m) for equipment with an operating frequency in the band between 24 kHz and 30 kHz;

 4. Forming beams of less than 1° on any axis and having an operating frequency of less than 100 kHz;

 5. Designed to operate with an unambiguous display range exceeding 5,120 m; or

6A001 a. 1. continued

 

 6. Designed to withstand pressure during normal operation at depths exceeding 1,000 m and having transducers with any of the following:

 a. Dynamic compensation for pressure; or

 b. Incorporating other than lead zirconate titanate as the transduction element;

 

 c. Acoustic projectors, including transducers, incorporating piezoelectric, magnetostrictive, electrostrictive, electrodynamic or hydraulic elements operating individually or in a designed combination and having any of the following:

 Note 1: The control status of acoustic projectors, including transducers, specially designed for other equipment is determined by the control status of the other equipment.

 Note 2: 6A001.a.1.c. does not control electronic sources which direct the sound vertically only, or mechanical (e.g., air gun or vapourshock gun) or chemical (e.g., explosive) sources.

 1. An instantaneous radiated ‘acoustic power density’ exceeding 0.01 mW/mm2/Hz for devices operating at frequencies below 10 kHz;

 2. A continuously radiated ‘acoustic power density’ exceeding 0.001 mW/mm2/Hz for devices operating at frequencies below 10 kHz; or

 Technical Note:

 ‘Acoustic power density’ is obtained by dividing the output acoustic power by the product of the area of the radiating surface and the frequency of operation.

 3. Sidelobe suppression exceeding 22 dB;

 

 d. Acoustic systems, equipment and specially designed components for determining the position of surface vessels or underwater vehicles designed to operate at a range exceeding 1,000 m with a positioning accuracy of less than 10 m rms (root mean square) when measured at a range of 1,000 m;

 Note: 6A001.a.1.d. includes:

  a. Equipment using coherent “signal processing” between two or more beacons and the hydrophone unit carried by the surface vessel or underwater vehicle;

  b. Equipment capable of automatically correcting speedofsound propagation errors for calculation of a point.

6A001 a. continued

 

 2. Passive (receiving, whether or not related in normal application to separate active equipment) systems, equipment and specially designed components therefor, as follows:

 

 a. Hydrophones having any of the following:

 Note: The control status of hydrophones specially designed for other equipment is determined by the control status of the other equipment.

 

 1. Incorporating continuous flexible sensing elements;

 

 2. Incorporating flexible assemblies of discrete sensing elements with either a diameter or length less than 20 mm and with a separation between elements of less than 20 mm;

 

 3. Having any of the following sensing elements:

 a. Optical fibres;

 b. ‘Piezoelectric polymer films’ other than polyvinylidenefluoride (PVDF) and its copolymers {P(VDFTrFE) and P(VDFTFE)}; or

 c. ‘Flexible piezoelectric composites’;

 

 4. A ‘hydrophone sensitivity’ better than 180 dB at any depth with no acceleration compensation;

 

 5. Designed to operate at depths exceeding 35 m with acceleration compensation; or

 

 6. Designed for operation at depths exceeding 1,000 m;

 

 Technical Notes:

 1. ‘Piezoelectric polymer film’ sensing elements consist of polarised polymer film that is stretched over and attached to a supporting frame or spool (mandrel).

 2. ‘Flexible piezoelectric composite’ sensing elements consist of piezoelectric ceramic particles or fibres combined with an electrically insulating, acoustically transparent rubber, polymer or epoxy compound, where the compound is an integral part of the sensing elements.

 3. ‘Hydrophone sensitivity’ is defined as twenty times the logarithm to the base 10 of the ratio of rms output voltage to a 1 V rms reference, when the hydrophone sensor, without a preamplifier, is placed in a plane wave acoustic field with an rms pressure of 1 µPa.  For example, a hydrophone of      160 dB (reference 1 V per µPa) would yield an output voltage of 108 V in such a field, while one of 180 dB sensitivity would yield only 109 V output. Thus, 160 dB is better than 180 dB.

 

6A001 a. 2. continued

 

 b. Towed acoustic hydrophone arrays having any of the following:

 1. Hydrophone group spacing of less than 12.5 m or ‘able to be modified’ to have hydrophone group spacing of less than 12.5 m;

 2. Designed or ‘able to be modified’ to operate at depths exceeding 35 m;

 Technical Note:

 ‘Able to be modified’ in 6A001.a.2.b.1. and 2. means having provisions to allow a change of the wiring or interconnections to alter hydrophone group spacing or operating depth limits. These provisions are: spare wiring exceeding 10% of the number of wires, hydrophone group spacing adjustment blocks or internal depth limiting devices that are adjustable or that control more than one hydrophone group.

 3. Heading sensors specified in 6A001.a.2.d.;

 4. Longitudinally reinforced array hoses;

 5. An assembled array of less than 40 mm in diameter; or

 6. Deleted;

 7. Hydrophone characteristics specified in 6A001.a.2.a.;

 

 c. Processing equipment, specially designed for towed acoustic hydrophone arrays, having “user accessible programmability” and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beam forming using Fast Fourier or other transforms or processes;

 

 d. Heading sensors having all of the following:

 1. An accuracy of better than ± 0.5°; and

 2. Designed to operate at depths exceeding 35 m or having an adjustable or removable depth sensing device in order to operate at depths exceeding 35 m;

 

 e. Bottom or bay cable systems having any of the following:

 1. Incorporating hydrophones specified in 6A001.a.2.a.; or

 2. Incorporating multiplexed hydrophone group signal modules having all of the following characteristics:

 a. Designed to operate at depths exceeding 35 m or having an adjustable or removable depth sensing device in order to operate at depths exceeding 35 m; and

 b. Capable of being operationally interchanged with towed acoustic hydrophone array modules;

 

6A001 a. 2. continued

 

 f. Processing equipment, specially designed for bottom or bay cable systems, having “user accessible programmability” and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beam forming using Fast Fourier or other transforms or processes;

 

 b. Correlationvelocity and Dopplervelocity sonar log equipment, designed to measure the horizontal speed of the equipment carrier relative to the sea bed, as follows:

 

 1. Correlationvelocity sonar log equipment having any of the following characteristics:

 a. Designed to operate at distances between the carrier and the sea bed exceeding 500 m; or

 b. Having speed accuracy better than 1% of speed;

 

 2. Dopplervelocity sonar log equipment having speed accuracy better than 1% of speed.

 

 Note 1: 6A001.b. does not control depth sounders limited to any of the following:

  1. Measuring the depth of water;
  2. Measuring the distance of submerged or buried objects; or
  3. Fish finding.

 

 Note 2: 6A001.b. does not control equipment specially designed for installation on surface vessels.

 

 

6A002 Optical sensors or equipment and components therefor, as follows:

 N.B.: SEE ALSO 6A102.

 

 a. Optical detectors as follows:

 

 1. “Spacequalified” solidstate detectors as follows:

 

 a. “Spacequalified” solidstate detectors having all of the following:

 1. A peak response in the wavelength range exceeding 10 nm but not exceeding 300 nm; and

 2. A response of less than 0.1% relative to the peak response at a wavelength exceeding 400 nm;

 

 b. “Spacequalified” solidstate detectors having all of the following:

 1. A peak response in the wavelength range exceeding 900 nm but not exceeding 1,200 nm; and

 2. A response “time constant” of 95 ns or less;

 

 

 

6A002 a. 1. continued

 

 c. “Spacequalified” solidstate detectors having a peak response in the wavelength range exceeding 1,200 nm but not exceeding 30,000 nm;

 

 2. Image intensifier tubes and specially designed components therefor, as follows:

 

 Note: 6A002.a.2. does not control nonimaging photomultiplier tubes having an electron sensing device in the vacuum space limited solely to any of the following:

  1. A single metal anode; or
  2. Metal anodes with a centre to centre spacing greater than 500 µm.

 

 Technical Note:

 ‘Charge multiplication’ is a form of electronic image amplification and is defined as the generation of charge carriers as a result of an impact ionization gain process. ‘Charge multiplication’ sensors may take the form of an image intensifier tube, solid state detector or “focal plane array”.

 

 a. Image intensifier tubes having all of the following:

 1. A peak response in the wavelength range exceeding 400 nm but not exceeding 1,050 nm;

 2. a. A microchannel plate with a hole pitch (centretocentre spacing) of 12 µm or less; or

 b. An electron sensing device with a nonbinned pixel pitch of 500 µm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate; and

 3. Any of the following photocathodes:

 a. S20, S25 or multialkali photocathodes with a luminous sensitivity exceeding 350 µA/lm;

 b. GaAs or GaInAs photocathodes; or

 c. Other “IIIV” compound semiconductor photocathodes;

 Note: 6A002.a.2.a.3.c. does not  apply to compound semiconductor photocathodes with a  maximum radiant sensitivity of 10 mA/W or less.

 

 b. Image intensifier tubes having all of the following:

 1. A peak response in the wavelength range exceeding 1,050 nm but not exceeding 1,800 nm;

 2. Electron image amplification using any of the following:

 a. A microchannel plate with a hole pitch (centretocentre spacing) of 12 µm or less; or

 

 

 

6A002 a. 2. continued

 

 b. An electron sensing device with a nonbinned pixel pitch of 500 µm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate; and

 3. IIIV compound semiconductor (e.g., GaAs or GaInAs) photocathodes and transferred electron photocathodes;

 Note: 6A002.a.2.b.3. does not control compound semiconductor photocathodes with a maximum radiant sensitivity of 15 mA/W or less.

 

 c. Specially designed components as follows:

 1. Microchannel plates having a hole pitch (centretocentre spacing) of 12 µm or less;

 2. An electron sensing device with a nonbinned pixel pitch of 500 µm or less, specially designed or modified to achieve ‘charge multiplication’ other than by a microchannel plate;

 3. IIIV compound semiconductor (e.g., GaAs or GaInAs) photocathodes and transferred electron photocathodes;

 Note: 6A002.a.2.c.3. does not control compound semiconductor photocathodes designed to achieve a maximum radiant sensitivity of any of the following:

  1. 10 mA/W or less at the peak response in the wavelength range exceeding 400 nm but not exceeding 1,050 nm; or
  2. 15 mA/W or less at the peak response in the wavelengthrange exceeding 1,050 nm but not exceeding 1,800 nm.

 

 3. Non“spacequalified” “focal plane arrays” as follows:

 

 N.B.: ‘Microbolometer’ non”spacequalified” “focal plane arrays” are only specified in 6A002.a.3.f.

 

 Technical Notes:

Linear or twodimensional multielement detector arrays are referred to as “focal plane arrays”;

 

 Note 1: 6A002.a.3. includes photoconductive arrays and photovoltaic arrays.

 

 Note 2: 6A002.a.3. does not control:

  a. Multielement (not to exceed 16 elements) encapsulated photoconductive cells using either lead sulphide or lead selenide;

  b. Pyroelectric detectors using any of the following:

   1.  Triglycine sulphate and variants;

   2.  Leadlanthanumzirconium titanate and variants;

   3.  Lithium tantalate;

6A002 a. 3. continued

 

   4.  Polyvinylidene fluoride and variants; or

   5.  Strontium barium niobate and variants.

  c. “Focal plane arrays” specially designed or modified to achieve ‘charge multiplication’ and limited by design to have a maximum radiant sensitivity of 10 mA/W or less for wavelengths exceeding 760 nm, having all of the following:

  1. Incorporating a response limiting mechanism designed not to be removed or modified; and

  2. Any of the following:

  a. The response limiting mechanism is integral to or combined with the detector element; or

  b. The “focal plane array” is only operable with the response limiting mechanism in place.

 Technical Note:

 A response limiting mechanism integral to the detector element is designed not to be removed or modified without rendering the detector inoperable.

 

 Technical Note:

 ‘Charge multiplication’ is a form of electronic image amplification and is defined as the generation of charge carriers as a result of an impact ionization gain process. ‘Charge multiplication’ sensors may take the form of an image intensifier tube, solid state detector or “focal plane array”.

 

 a. Non“spacequalified” “focal plane arrays” having all of the following:

 1. Individual elements with a peak response within the wavelength range exceeding 900 nm but not exceeding 1,050 nm; and

 2. Any of the following:

 a. A response “time constant” of less than 0.5 ns; or

 b. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum radiant sensitivity exceeding 10 mA/W;

 

 b. Non“spacequalified” “focal plane arrays” having all of the following:

 1. Individual elements with a peak response in the wavelength range exceeding 1,050 nm but not exceeding 1,200 nm; and

 2. Any of the following:

 a. A response “time constant” of 95 ns or less; or

 b. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum radiant sensitivity exceeding 10 mA/W;

 

 

 

6A002 a. 3. continued

 

 c. Non“spacequalified” nonlinear (2dimensional) “focal plane arrays” having individual elements with a peak response in the wavelength range exceeding 1,200 nm but not exceeding 30,000 nm;

 

 N.B.:  Silicon and other material based ‘microbolometer’ non”spacequalified” “focal plane arrays” are only specified in 6A002.a.3.f.

 

 d. Non“spacequalified” linear (1dimensional) “focal plane arrays” having all of the following:

 1. Individual elements with a peak response in the wavelength range exceeding 1,200 nm but not exceeding 3,000 nm; and

 

 2. Any of the following:

 a. A ratio of ‘scan direction’ dimension of the detector element to the ‘crossscan direction’ dimension of the detector element of less than 3.8; or

 b. Signal Processing In The Element (SPRITE);

 Note: 6A002.a.3.d. does not control “focal plane arrays” (not to exceed 32 elements) having detector elements limited solely to germanium material.

 

 Technical Note:

 For the purposes of 6A002.a.3.d., ‘crossscan direction’ is defined as the axis parallel to the linear array of detector elements and the ‘scan direction’ is defined as the axis perpendicular to the linear array of detector elements.

 

 e. Non“spacequalified” linear (1dimensional) “focal plane arrays” having individual elements with a peak response in the wavelength range exceeding 3,000 nm but not exceeding 30,000 nm;

 

 f. Non“spacequalified” nonlinear (2dimensional) infrared “focal plane arrays” based on ‘microbolometer’ material having individual elements with an unfiltered response in the wavelength range equal to or exceeding 8,000 nm but not exceeding 14,000 nm;

 

 Technical Note:

For the purposes of 6A002.a.3.f., ‘microbolometer’ is defined as a thermal imaging detector that, as a result of a temperature change in the detector caused by the absorption of infrared radiation, is used to generate any usable signal.

 

 g. Non“spacequalified” “focal plane arrays” having all of the following:

 

6A002 a.3. continued

 

 1. Individual detector elements with a peak response in the wavelength range exceeding 400 nm but not exceeding 900 nm;

 2. Specially designed or modified to achieve ‘charge multiplication’ and having a maximum radiant sensitivity exceeding 10 mA/W for wavelengths exceeding 760 nm; and

 3. Greater than 32 elements.

 

 b. “Monospectral imaging sensors” and “multispectral imaging sensors” designed for remote sensing applications and having any of the following:

 1. An InstantaneousFieldOfView (IFOV) of less than 200  µrad (microradians); or

 

 2. Specified for operation in the wavelength range exceeding 400 nm but not exceeding 30,000 nm and having all the following:

 a. Providing output imaging data in digital format; and

 b. Having any of the following characteristics:

 1. “Spacequalified”; or

 2. Designed for airborne operation, using other than silicon detectors, and having an IFOV of less than 2.5 mrad (milliradians);

 

 c. ‘Direct view’ imaging equipment incorporating any of the following:

 1. Image intensifier tubes specified in 6A002.a.2.a. or 6A002.a.2.b.;

 2. “Focal plane arrays” specified in 6A002.a.3. or 6A002.e.; or

 3. Solid state detectors specified in 6A002.a.1.;

 Technical Note:

 ‘Direct view’ refers to imaging equipment that presents a visual image to a human observer without converting the image into an electronic signal for television display, and that cannot record or store the image photographically, electronically or by any other means.

 Note: 6A002.c. does not control equipment as follows, when incorporating other than GaAs or GaInAs photocathodes:

  a. Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems;

  b. Medical equipment;

  c. Industrial equipment used for inspection, sorting or analysis of the properties of materials;

  d. Flame detectors for industrial furnaces;

e.          Equipment specially designed for laboratory use.

 

 d. Special support components for optical sensors, as follows:

 1. “Spacequalified” cryocoolers;

 2. Non“spacequalified” cryocoolers having a cooling source temperature below 218 K (55°C), as follows:

 a. Closed cycle type with a specified MeanTimeToFailure (MTTF) or MeanTimeBetweenFailures (MTBF), exceeding 2,500 hours;

6A002 d. continued

 

 b. JouleThomson (JT) selfregulating minicoolers having bore (outside) diameters of less than 8 mm;

 3. Optical sensing fibres specially fabricated either compositionally or structurally, or modified by coating, to be acoustically, thermally, inertially, electromagnetically or nuclear radiation sensitive;

 

 e. “Space qualified” “focal plane arrays” having more than 2,048 elements per array and having a peak response in the wavelength range exceeding 300 nm but not exceeding 900 nm.

 

6A003 Cameras, systems or equipment, and components therefor, as follows:

 N.B.: SEE ALSO 6A203.

 N.B.: For cameras specially designed or modified for underwater use, see 8A002.d. and 8A002.e.

 

 a. Instrumentation cameras and specially designed components therefor, as follows:

 

 Note: Instrumentation cameras, specified in 6A003.a.3. to 6A003.a.5., with modular structures should be evaluated by their maximum capability, using plugins available according to the camera manufacturer’s specifications.

 

 1. Highspeed cinema recording cameras using any film format from 8 mm to 16 mm inclusive, in which the film is continuously advanced throughout the recording period, and that are capable of recording at framing rates exceeding 13,150 frames/s;

 Note: 6A003.a.1. does not control cinema recording cameras designed for civil purposes.

 2. Mechanical high speed cameras, in which the film does not move, capable of recording at rates exceeding 1,000,000 frames/s for the full framing height of 35 mm film, or at proportionately higher rates for lesser frame heights, or at proportionately lower rates for greater frame heights;

 3. Mechanical or electronic streak cameras, having writing speeds exceeding 10mm/s;

 4. Electronic framing cameras having a speed exceeding 1,000,000 frames/s;

 5. Electronic cameras having all of the following:

 a. An electronic shutter speed (gating capability) of less than 1 µs per full frame; and

 b. A read out time allowing a framing rate of more than 125 full frames per second.

 6. Plugins having all of the following characteristics:

 a. Specially designed for instrumentation cameras which have modular structures and which are specified in 6A003.a.; and

 b. Enabling these cameras to meet the characteristics specified in 6A003.a.3., 6A003.a.4., or 6A003.a.5., according to the manufacturer’s specifications;

 

6A003 continued

 

 b. Imaging cameras as follows:

 

 Note: 6A003.b. does not control television or video cameras specially designed for television broadcasting.

 

 1. Video cameras incorporating solid state sensors, having a peak response in the wavelength range exceeding 10  nm, but not exceeding 30,000 nm and having all of the following:

 a. Having any of the following:

 1. More than 4 x 106 “active pixels” per solid state array for monochrome (black and white) cameras;

 2. More than 4 x 106 “active pixels” per solid state array for colour cameras incorporating three solid state arrays; or

 3. More than 12 x 106 “active pixels” for solid state array colour cameras incorporating one solid state array; and

 b.  Having any of the following:

 1. Optical mirrors specified in 6A004.a.;

 2. Optical control equipment specified in 6A004.d.; or

 3. The capability for annotating internally generated ‘camera tracking data’;

 Technical Notes:

 1. For the purpose of this entry, digital video cameras should be evaluated by the maximum number of “active pixels” used for capturing moving images.

 2. For the purpose of this entry, ‘camera tracking data’ is the information necessary to define camera line of sight orientation with respect to the earth.  This includes: 1) the horizontal angle the camera line of sight makes with respect to the earth’s magnetic field direction and; 2) the vertical angle between the camera line of sight and the earth’s horizon.

 

 2. Scanning cameras and scanning camera systems, having all of the following:

 a. A peak response in the wavelength range exceeding 10 nm, but not exceeding 30,000 nm;

 b. Linear detector arrays with more than 8,192 elements per array; and

 c. Mechanical scanning in one direction;

 

 3. Imaging cameras incorporating image intensifier tubes specified in 6A002.a.2.a. or 6A002.a.2.b.;

 

 4. ‘Imaging cameras’ incorporating “focal plane arrays” having any of the following:

6A003 b. 4. continued

 

a. Incorporating “focal plane arrays” specified in 6A002.a.3.a. to 6A002.a.3.e.;

b. Incorporating “focal plane arrays” specified in 6A002.a.3.f.;

c. Incorporating “focal plane arrays” specified in 6A002.a.3.g.; or

d. Incorporating “focal plane arrays” specified in 6A002.e.;

 

 Note 1: Imaging cameras specified in 6A003.b.4 include “focal plane arrays” combined with sufficient “signal processing” electronics, beyond the read out integrated circuit, to enable as a minimum the output of an analogue or digital signal once power is supplied.

 

 Note 2: 6A003.b.4.a. does not control imaging cameras incorporating linear “focal plane arrays” with 12 elements or fewer, not employing timedelayandintegration within the element and designed for any of the following:

   a. Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems;

   b. Industrial equipment used for inspection or monitoring of heat flows in buildings, equipment or industrial processes;

   c. Industrial equipment used for inspection, sorting or analysis of the properties of materials;

   d. Equipment specially designed for laboratory use; or

   e. Medical equipment.

 

 Note 3: 6A003.b.4.b. does not control imaging cameras having any of the following characteristics:

   a.  A maximum frame rate equal to or less than 9 Hz;

   b.  Having all of the following:

    1. Having a minimum horizontal or vertical ‘InstantaneousFieldofView (IFOV)’ of at least 10 mrad/pixel (milliradians/pixel);

    2. Incorporating a fixed focallength lens that is not designed to be removed;

    3.  Not incorporating a ‘direct view’ display; and

    4.  Having any of the following:

     a.   No facility to obtain a viewable image of the detected fieldofview, or

     b.  The camera is designed for a single kind of application and designed not to be user modified; or

   c. The camera is specially designed for installation into a civilian passenger land vehicle of less than 3 tonnes (gross vehicle weight) and having all of the following:

    1. Is only operable when installed in any of the following:

     a. The civilian passenger land vehicle for which it was intended; or

 

6A003 b. continued

 

     b. A specially designed, authorized maintenance test facility; and

2. Incorporates an active mechanism that forces the camera not to function when it is removed from the vehicle for which it was intended.

 

  Technical Notes:

   1. ‘Instantaneous Field of View (IFOV)’ specified in 6A003.b.4. Note 3.b. is the lesser figure of the ‘Horizontal IFOV’ or the ‘Vertical IFOV’.

    ‘Horizontal IFOV’  =  horizontal Field of View (FOV) / number of horizontal detector elements

    ‘Vertical IFOV’  =  vertical Field of View (FOV) / number of vertical detector elements.

   2. ‘Direct view’ in 6A003.b.4. Note 3.b. refers to an imaging camera operating in the infrared spectrum that presents a visual image to a human observer using a neartoeye micro display incorporating any lightsecurity mechanism.

 

 Note 4: 6A003.b.4.c. does not control ‘imaging cameras’ having any of the following:

   a.  Having all of the following:

    1. Where the camera is specially designed for installation as an integrated component into indoor and wallplugoperated systems or equipment, limited by design for a single kind of application, as follows;

     a. Industrial process monitoring, quality control, or analysis of the properties of materials;

     b. Laboratory equipment specially designed for scientific research;

     c. Medical equipment;

     d. Financial fraud detection equipment; and

    2. Is only operable when installed in any of the following:

     a. The system(s) or equipment for which it was intended; or

     b. A specially designed, authorised maintenance facility; and

    3. Incorporates an active mechanism that forces the camera not to function when it is removed from the system(s) or equipment for which it was intended;

   b. Where the camera is specially designed for installation into a civilian passenger land vehicle of less than three tonnes (gross vehicle weight), or passenger and vehicle ferries having a length overall (LOA) 65 m or greater, and having all of the following:

6A003 b. continued

 

    1. Is only operable when installed in any of the following:

     a. The civilian passenger land vehicle or passenger and vehicle ferry for which it was intended; or

     b. A specially designed, authorised maintenance test facility; and

    2. Incorporates an active mechanism that forces the camera not to function when it is removed from the vehicle for which it was intended;

   c. Limited by design to have a maximum radiant sensitivity of 10 mA/W or less for wavelengths exceeding 760 nm, having all of the following:

    1. Incorporating a response limiting mechanism designed not to be removed or modified; and

    2. Incorporates an active mechanism that forces the camera not to function when the response limiting mechanism is removed; or

   d. Having all of the following:

    1. Not incorporating a ‘direct view’ or electronic image display;

    2. Has no facility to output a viewable image of the detected field of view;

    3. The “focal plane array” is only operable when installed in the camera for which it was intended; and

    4. The “focal plane array” incorporates an active mechanism that forces it to be permanently inoperable when removed from the camera for which it was intended.

 

 b. 5. Imaging cameras incorporating solidstate detectors specified by 6A002.a.1.

 

 

6A004 Optical equipment and components, as follows:

 

 a. Optical mirrors (reflectors) as follows:

N.B.: For optical mirrors specially designed for lithography equipment, see 3B001.

 1. “Deformable mirrors” having either continuous or multielement surfaces, and specially designed components therefor, capable of dynamically repositioning portions of the surface of the mirror at rates exceeding 100 Hz;

 2. Lightweight monolithic mirrors having an average “equivalent density” of less than 30 kg/m2 and a total mass exceeding 10 kg;

 

 

6A004 a. continued

 

 3. Lightweight “composite” or foam mirror structures having an average “equivalent density” of less than 30 kg/m2 and a total mass exceeding 2 kg;

 4. Beam steering mirrors more than 100 mm  in diameter or length of major axis, which maintain a flatness of λ/2 or better (λ is equal to 633 nm) having a control bandwidth exceeding 100 Hz;

 

 b. Optical components made from zinc selenide (ZnSe) or zinc sulphide (ZnS) with transmission in the wavelength range exceeding 3,000 nm but not exceeding 25,000 nm and having any of the following:

 1. Exceeding 100 cm3 in volume; or

 2. Exceeding 80 mm in diameter or length of major axis and 20 mm in thickness (depth);

 

 c. “Spacequalified” components for optical systems, as follows:

 1. Lightweighted to less than 20% “equivalent density” compared with a solid blank of the same aperture and thickness;

 

 2. Raw substrates, processed substrates having surface coatings (singlelayer or multilayer, metallic or dielectric, conducting, semiconducting or insulating) or having protective films;

 

 3. Segments or assemblies of mirrors designed to be assembled in space into an optical system with a collecting aperture equivalent to or larger than a single optic 1 m in diameter;

 

 4. Manufactured from “composite” materials having a coefficient of linear thermal expansion equal to or less than 5 x 106 in any coordinate direction;

 

 d. Optical control equipment as follows:

 1. Specially designed to maintain the surface figure or orientation of the “spacequalified” components specified in 6A004.c.1. or 6A004.c.3.;

 

 2. Having steering, tracking, stabilisation or resonator alignment bandwidths equal to or more than 100 Hz and an accuracy of 10 µrad (microradians) or less;

 

 3. Gimbals having all of the following:

 a. A maximum slew exceeding 5°;

 b. A bandwidth of 100 Hz or more;

 c. Angular pointing errors of 200 µrad (microradians) or less; and

 d. Having any of the following:

 1. Exceeding 0.15 m but not exceeding 1 m in diameter or major axis length and capable of angular accelerations exceeding 2 rad (radians)/s2; or

 

 

6A004 d. continued

 

 2. Exceeding 1 m in diameter or major axis length and capable of angular accelerations exceeding 0.5 rad (radians)/s2;

 

 4. Specially designed to maintain the alignment of phased array or phased segment mirror systems consisting of mirrors with a segment diameter or major axis length of 1 m or more;

 

 e. ‘Aspheric optical elements’ having all of the following:

 1. Largest dimension of the opticalaperture greater than 400 mm;

 2. Surface roughness less than 1 nm (rms) for sampling lengths equal to or greater than 1 mm; and

 3. Coefficient of linear thermal expansion’s absolute magnitude less than 3x106/K at 25°C.

 Technical Notes:

 1. An ‘aspheric optical element’ is any element used in an optical system whose imaging surface or surfaces are designed to depart from the shape of an ideal sphere.

 

 2. Manufacturers are not required to measure the surface roughness listed in 6A004.e.2. unless the optical element was designed or manufactured with the intent to meet, or exceed, the control parameter.

 

 Note 6A004.e. does not control aspheric optical elements having any of the following:

  a. Largest opticalaperture dimension less than 1 m and focal length to aperture ratio equal to or greater than 4.5:1;

  b. Largest opticalaperture dimension equal to or greater than 1 m and focal length to aperture ratio equal to or greater than 7:1;

  c. Designed as Fresnel, flyeye, stripe, prism or diffractive optical elements;

  d. Fabricated from borosilicate glass having a coefficient of linear thermal expansion greater than 2.5x106 /K at 25 °C; or

  e. An xray optical element having inner mirror capabilities (e.g., tubetype mirrors).

 

 N.B.: For aspheric optical elements specially designed for lithography equipment, see 3B001.

 

 

6A005 “Lasers”, other than those specified in 0B001.g.5. or 0B001.h.6., components and optical equipment, as follows:

 N.B.: SEE ALSO 6A205.

 

 Note 1: Pulsed “lasers” include those that run in a continuous wave (CW) mode with pulses superimposed.

 Note 2: Excimer, semiconductor, chemical, CO, CO2, and nonrepetitive pulsed Nd:glass “lasers” are only specified in 6A005.d.

6A005 continued

 

 Note 3: 6A005 includes fibre “lasers”.

 Note 4: The control status of “lasers” incorporating frequency conversion (i.e., wavelength change) by means other than one “laser” pumping another “laser” is determined by applying the control parameters for both the output of the source “laser” and the frequencyconverted optical output.

 Note 5: 6A005 does not control “lasers” as follows:

  a. Ruby with output energy below 20 J;

  b. Nitrogen;

  c. Krypton.

 

 Technical Note:

 In 6A005 ‘Wallplug efficiency’ is defined as the ratio of “laser” output power (or “average output power”) to total electrical input power required to operate the “laser”, including the power supply/conditioning and thermal conditioning/heat exchanger.

 

 a. Non”tunable” continuous wave “(CW) lasers” having any of the following:

 1. Output wavelength less than 150 nm and output power exceeding 1 W;

 

 2.  Output wavelength of 150 nm or more but not exceeding 520 nm and output power exceeding 30 W;

  Note:  6A005.a.2. does not control Argon “lasers” having an output power equal to or less than 50 W.

 

 3. Output wavelength exceeding 520 nm but not exceeding 540 nm and any of the following:

 a. Single transverse mode output and output power exceeding 50 W; or

 b. Multiple transverse mode output and output power exceeding 150 W;

 

 4. Output wavelength exceeding 540 nm but not exceeding 800 nm and output power exceeding 30 W;

 

 5. Output wavelength exceeding 800 nm but not exceeding 975 nm and any of the following:

 a. Single transverse mode output and output power exceeding 50 W; or

 b. Multiple transverse mode output and output power exceeding 80 W;

 

 6. Output wavelength exceeding 975 nm but not exceeding 1,150 nm and any of the following:

 a. Single transverse mode output and any of the following:

 1. ‘Wallplug efficiency exceeding 12% and output power exceeding 100 W; or

2. Output power exceeding 150 W; or

 b. Multiple transverse mode output and any of the following:

6A005 a. continued

 

 1. Wallplug efficiency exceeding 18% and output power exceeding 500 W; or

2. Output power exceeding 2 kW;

 Note: 6A005.a.6.b. does not control multiple transverse mode, industrial “lasers” with output power exceeding 2 kW and

  not exceeding 6 kW with a total mass greater than 1,200 kg.  For the purpose of this note, total mass includes all components required to operate the “laser”, e.g., “laser”, power supply, heat exchanger, but excludes external optics for beam conditioning and/or delivery.

 

 7. Output wavelength exceeding 1,150 nm but not exceeding 1,555 nm and of the following:

 a. Single transverse mode and output power exceeding 50 W; or

 b. Multiple transverse mode and output power exceeding 80 W; or

 

 8. Output wavelength exceeding 1,555 nm and output power exceeding 1 W;

 

 b. Non”tunable” “pulsed lasers” having any of the following:

 

 1. Output wavelength less than 150 nm and any of the following:

 a. Output energy exceeding 50 mJ per pulse and “peak power” exceeding 1 W; or

 b. “Average output power” exceeding 1 W;

 

 2. Output wavelength of 150 nm or more but not exceeding 520 nm and any of the following:

 a. Output energy exceeding 1.5 J per pulse and “peak power” exceeding 30 W; or

 b. “Average output power” exceeding 30 W;

 Note: 6A005.b.2.b. does not control Argon “lasers” having an “average output power” equal to or less than 50 W.

 

 3. Output wavelength exceeding 520 nm but not exceeding 540 nm and any of the following:

 a. Single transverse mode output and any of the following:

 1. Output energy exceeding 1.5 J per pulse and “peak power” exceeding 50 W; or

2. “Average output power” exceeding 50 W; or

 b. Multiple transverse mode output and any of the following:

 1. Output energy exceeding 1.5 J per pulse and “peak power” exceeding 150 W; or

 2. “Average output power” exceeding 150 W;


6A005 b. continued

 

 4. Output wavelength exceeding 540 nm but not exceeding 800 nm and any of the following:

 a. Output energy exceeding 1.5 J per pulse and “peak power” exceeding 30 W; or

 b. “Average output power” exceeding 30 W;

 

 5. Output wavelength exceeding 800 nm but not exceeding 975 nm and any of the following:

 a. “Pulse duration” not exceeding 1 µs and any of the following:

 1. Output energy exceeding 0.5 J per pulse and “peak power” exceeding 50 W;

 2. Single transverse mode output and “average output power” exceeding 20 W; or

 3. Multiple transverse mode output and “average output power” exceeding 50 W; or

 b. “Pulse duration” exceeding 1 µs and any of the following:

 1. Output energy exceeding 2 J per pulse and “peak power” exceeding 50 W;

 2. Single transverse mode output and “average output power” exceeding 50 W; or

 3. Multiple transverse mode output and “average output power” exceeding 80 W;

 

 6. Output wavelength exceeding 975 nm but not exceeding 1,150 nm and any of the following:

 a. “Pulse duration” of less than 1 ns and any of the following:

 1. Output “peak power” exceeding 5 GW per pulse;

 2. “Average output power” exceeding 10 W; or

 3. Output energy exceeding 0.1 J per pulse;

 b. “Pulse duration” exceeding 1 ns but not exceeding 1 µs, and any of the following:

 1. Single transverse mode output and any of the following:

 a. “Peak power” exceeding 100 MW;

 b. “Average output power” exceeding 20 W limited by design to a maximum pulse repetition frequency less than or equal to 1 kHz;

 c. Wallplug efficiency exceeding 12%, “average output power” exceeding 100 W and capable of operating at a pulse repetition frequency greater than 1 kHz;

 d. “Average output power” exceeding 150 W and capable of operating at a pulse repetition frequency greater than 1 kHz; or

 e. Output energy exceeding 2 J per pulse; or

 2. Multiple transverse mode output and any of the following:

 a. “Peak power” exceeding 400 MW;

 b. ‘Wallplug efficiency exceeding 18% and “average output power” exceeding 500 W;

 c. “Average output power” exceeding 2 kW; or

6A005 b. 6. continued

 

 d. Output energy exceeding 4 J per pulse; or

 

 c. “Pulse duration” exceeding 1 µs and any of the following:

 1. Single transverse mode output and any of the following:

 a. “Peak power” exceeding 500 kW;

 b. ‘Wallplug efficiency exceeding 12% and “average output power” exceeding 100 W; or

 c. “Average output power” exceeding 150 W; or

 2. Multiple transverse mode output and any of the following:

 a. “Peak power” exceeding 1 MW;

 

 b. ‘Wallplug efficiency exceeding 18% and “average output power” exceeding 500 W; or

 c. “Average output power” exceeding 2 kW;

 

 7. Output wavelength exceeding 1,150 nm but not exceeding 1,555 nm, and any of the following:

 a. “Pulse duration” not exceeding 1 µs and any of the following:

 1. Output energy exceeding 0.5 J per pulse and “peak power” exceeding 50 W;

 2. Single transverse mode output and “average output power” exceeding 20 W; or

 3. Multiple transverse mode output and “average output power” exceeding 50 W; or

 b. “Pulse duration” exceeding 1 µs and any of the following:

 1. Output energy exceeding 2 J per pulse and “peak power” exceeding 50 W;

 2. Single transverse mode output and “average output power” exceeding 50 W; or

 3. Multiple transverse mode output and “average output power” exceeding 80 W; or

 

 8. Output wavelength exceeding 1,555 nm and any of the following:

 a. Output energy exceeding 100 mJ per pulse and “peak power” exceeding 1 W; or

 b. “Average output power” exceeding 1 W;

 

 c. Tunable” “lasers” having any of the following:

 Note: 6A005.c. includes titanium–sapphire (Ti: Al2O3), thuliumYAG (Tm: YAG), thuliumYSGG (Tm: YSGG), alexandrite (Cr: BeAl2O4), colour centre “lasers”, dye “lasers”, and liquid “lasers”.

 

 1. Output wavelength less than 600 nm and any of the following:

 a. Output energy exceeding 50 mJ per pulse and “peak power” exceeding 1 W; or

 b. Average or CW output power exceeding 1 W;

 

 

6A005 c.continued

 

 2. Output wavelength of 600 nm or more but not exceeding 1,400 nm, and any of the following:

 a. Output energy exceeding 1 J per pulse and “peak power” exceeding 20 W; or

 b. Average or CW output power exceeding 20 W; or

 

 3. Output wavelength exceeding 1,400 nm and any of the following:

 a. Output energy exceeding 50 mJ per pulse and “peak power” exceeding 1 W; or

 b. Average or CW output power exceeding 1 W;

 

 d. Other “lasers”, not specified in 6A005.a., 6A005.b. or 6A005.c. as follows:

 

 1. Semiconductor “lasers” as follows:

 Note 1: 6A005.d.1. includes semiconductor “lasers” having optical output connectors (e.g., fibre optic pigtails).

 Note 2: The control status of semiconductor “lasers” specially designed for other equipment is determined by the control status of the other equipment.

 

 a. Individual singletransverse mode semiconductor “lasers” having any of the following:

 1. Wavelength equal to or less than 1,510 nm and average or CW output power, exceeding 1.5 W; or

 2. Wavelength greater than 1,510 nm and average or CW output power, exceeding 500 mW;

 

 b. Individual, multipletransverse mode semiconductor “lasers” having any of the following:

 1. Wavelength of less than 1,400 nm and average or CW output power, exceeding 10W;

 2. Wavelength equal to or greater than 1,400 nm and less than 1,900 nm and average or CW output power, exceeding 2.5 W; or

 3. Wavelength equal to or greater than 1,900 nm and average or CW output power, exceeding 1 W;

 

 c. Individual semiconductor “laser” ‘arrays’, having any of the following:

 1. Wavelength of less than 1,400 nm and average or CW output power, exceeding 80 W;

 2. Wavelength equal to or greater than 1,400 nm and less than 1,900 nm and average or CW output power, exceeding 25 W; or

 3. Wavelength equal to or greater than 1,900 nm and average or CW output power, exceeding 10 W;

 

 d. Array stacks of semiconductor “lasers” containing at least one array specified in 6A005.d.1.c.;

6A005 d. continued

 

 Technical Notes:

1. Semiconductor “lasers” are commonly called “laser” diodes.

2. An ‘array’ consists of multiple semiconductor “laser” emitters fabricated as a single chip so that the centres of the emitted light beams are on parallel paths.

3. An ‘array stack’ is fabricated by stacking, or otherwise assembling, ‘arrays’ so that the centres of the emitted light beams are on parallel paths.

 

 2. Carbon monoxide (CO) “lasers” having any of the following:

 a. Output energy exceeding 2 J per pulse and “peak power” exceeding 5 kW; or

 b. Average or CW output power exceeding 5 kW;

 

 3. Carbon dioxide (CO2) “lasers” having any of the following:

 a. CW output power exceeding 15 kW;

 b. Pulsed output with a “pulse duration” exceeding 10 µs and  any of the following:

 1. “Average output power” exceeding 10 kW; or

 2. “Peak power” exceeding 100 kW; or

 c. Pulsed output with a “pulse duration” equal to or less than 10 µs and any of the following:

 1. Pulse energy exceeding 5 J per pulse; or

 2. “Average output power” exceeding 2.5 kW;

 

 4. Excimer “lasers” having any of the following:

 a. Output wavelength not exceeding 150 nm and any of the following:

 1. Output energy exceeding 50 mJ per pulse; or

 2. “Average output power” exceeding 1 W;

 b. Output wavelength exceeding 150 nm but not exceeding 190 nm and any of the following:

 1. Output energy exceeding 1.5 J per pulse; or

 2. “Average output power” exceeding 120 W;

 c. Output wavelength exceeding 190 nm but not exceeding 360 nm and any of the following:

 1. Output energy exceeding 10 J per pulse; or

 2. “Average output power” exceeding 500 W; or

 d. Output wavelength exceeding 360 nm and any of the following:

 1. Output energy exceeding 1.5 J per pulse; or

 2. “Average output power” exceeding 30 W;

 

 N.B.: For excimer “lasers” specially designed for lithography equipment, see 3B001.

 

 5. “Chemical lasers” as follows:

 a. Hydrogen Fluoride (HF) “lasers”;

 b. Deuterium Fluoride (DF) “lasers”;

 c. “Transfer lasers” as follows:

6A005 d. continued

 

 1. Oxygen Iodine (O2I) “lasers”;

 2. Deuterium FluorideCarbon dioxide (DFCO2) “lasers”;

 

 6. Nonrepetitive pulsed Nd: glass “lasers” having any of the following:

 a. “Pulse duration” not exceeding 1 µs and output energy exceeding 50 J per pulse; or

 b. “Pulse duration” exceeding 1 µs and output energy exceeding 100 J per pulse;

 

 Note: Nonrepetitive pulsed refers to “lasers” that produce either a single output pulse or that have a time interval between pulses exceeding one minute.

 

 e. Components as follows:

 

 1. Mirrors cooled either by ‘active cooling’ or by heat pipe cooling;

  Technical Note:

  ‘Active cooling’ is a cooling technique for optical components using flowing fluids within the subsurface (nominally less than 1 mm below the optical surface) of the optical component to remove heat from the optic.

 

 2. Optical mirrors or transmissive or partially transmissive optical or electrooptical components, specially designed for use with specified “lasers”;

 

 f. Optical equipment as follows:

 

 N.B.: For shared aperture optical elements, capable of operating in “SuperHigh Power Laser” (“SHPL”) applications, see the Military Goods Lists.

 

 1. Dynamic wavefront (phase) measuring equipment capable of mapping at least 50 positions on a beam wavefront and any of the following:

 a. Frame rates equal to or more than 100 Hz and phase discrimination of at least 5% of the beam’s wavelength; or

 b. Frame rates equal to or more than 1,000 Hz and phase discrimination of at least 20% of the beam’s wavelength;

 

 2. “Laser” diagnostic equipment capable of measuring “SHPL” system angular beam steering errors of equal to or less than 10 µrad;

 

 3. Optical equipment and components, specially designed for a phasedarray “SHPL” system for coherent beam combination to an accuracy of λ/10 at the designed wavelength, or 0.1 µm, whichever is the smaller;

 

  4. Projection telescopes specially designed for use with “SHPL” systems.

 

6A006 “Magnetometers”, “magnetic gradiometers”, “intrinsic magnetic gradiometers”, underwater electric field sensors, “compensation systems”, and specially designed components therefor, as follows:

 

 Note: 6A006 does not control instruments specially designed for fishery applications or biomagnetic measurements for medical diagnostics.

 

 a. “Magnetometers” and subsystems as follows:

 

 1. Using “superconductive” (SQUID) “technology” and having any of the following:

 a. SQUID systems designed for stationary operation, without specially designed subsystems designed to reduce inmotion noise, and having a “noise level” (sensitivity) equal to or lower (better) than 50 fT (rms) per square root Hz at a frequency of 1 Hz; or

 b. SQUID systems having an inmotionmagntometer “noise level” (sensitivity) lower (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz and specially designed to reduce inmotion noise;

 

 2. Using optically pumped or nuclear precession (proton/Overhauser) “technology” having a “noise level” (sensitivity) lower (better) than 20 pT (rms) per square root Hz;

 

 3. Using fluxgate “technology” having a “noise level” (sensitivity) equal to or lower (better) than 10 pT (rms) per square root Hz at a frequency of 1 Hz;

 

 4. Induction coil “magnetometers” having a “noise level” (sensitivity) lower (better) than any of the following:

 a. 0.05 nT (rms) per square root Hz at frequencies of less than 1 Hz;

 b. 1 x 103 nT (rms) per square root Hz at frequencies of 1 Hz or more but not exceeding 10 Hz; or

 c. 1 x 104 nT (rms) per square root Hz at frequencies exceeding 10 Hz;

 

 5. Fibre optic “magnetometers” having a “noise level” (sensitivity) lower (better) than 1 nT (rms) per square root Hz;

 

 b. Underwater electric field sensors having a “noise level” (sensitivity) lower (better) than 8 nanovolt per metre per square root Hz when measured at 1 Hz;

 

 c. “Magnetic gradiometers” as follows:

 1. “Magnetic gradiometers” using multiple “magnetometers” specified in 6A006.a.;

 2. Fibre optic “intrinsic magnetic gradiometers” having a magnetic gradient field “noise level” (sensitivity) lower (better) than 0.3 nT/m rms per square root Hz;

6A006 c. continued

 

 3. “Intrinsic magnetic gradiometers”, using “technology” other than fibreoptic “technology”, having a magnetic gradient field “noise level” (sensitivity) lower (better) than 0.015 nT/m rms per square root Hz;

 d. “Compensation systems” for magnetic or underwater electric field sensors resulting in a performance equal to or better than the specified parameters of 6A006.a., 6A006.b. or 6A006.c.

 

 

6A007 Gravity meters (gravimeters) and gravity gradiometers, as follows:

 N.B.: SEE ALSO 6A107.

 

 a. Gravity meters designed or modified for ground use and having a static accuracy of less (better) than 10 µgal;

 Note: 6A007.a. does not control ground gravity meters of the quartz element (Worden) type.

 

 b. Gravity meters designed for mobile platforms and having all of the following:

 1. A static accuracy of less (better) than 0.7 mgal; and

 2. An inservice (operational) accuracy of less (better) than 0.7 mgal having a timetosteadystate registration of less than 2 minutes under any combination of attendant corrective compensations and motional influences;

 

 c. Gravity gradiometers.

 

 

6A008 Radar systems, equipment and assemblies having any of the following, and specially designed components therefor:

 N.B.: SEE ALSO 6A108.

 

 Note: 6A008 does not control:

   Secondary surveillance radar (SSR);

   Civil Automotive Radar;

   Displays or monitors used for air traffic control  (ATC) having no more than 12 resolvable elements per mm;

   Meteorological (weather) radar.

 

  1. Operating at frequencies from 40 GHz to 230 GHz and having any of the following:

 1. An average output power exceeding 100 mW; or

 2. Locating accuracy of 1 m or less (better) in range and 0.2 degree or less (better) in azimuth;

 

 b. A tunable bandwidth exceeding ± 6.25% of the ‘centre operating frequency’;

 

 

6A008 continued

 

  Technical Note:

 The ‘centre operating frequency’ equals one half of the sum of the highest plus the lowest specified operating frequencies.

 

 c. Capable of operating simultaneously on more than two carrier frequencies;

 

 d. Capable of operating in synthetic aperture (SAR), inverse synthetic aperture (ISAR) radar mode, or sidelooking airborne (SLAR) radar mode;

 

 e. Incorporating “electronically steerable phased array antennae”;

 

 f. Capable of heightfinding noncooperative targets;

 Note: 6A008.f. does not control precision approach radar (PAR) equipment conforming to ICAO standards.

 

 g. Specially designed for airborne (balloon or airframe mounted) operation and having Doppler “signal processing” for the detection of moving targets;

 

 h. Employing processing of radar signals and using any of the following:

 1. “Radar spread spectrum” techniques; or

 2. “Radar frequency agility” techniques;

 

 i. Providing groundbased operation with a maximum “instrumented range” exceeding 185 km;

 Note: 6A008.i. does not control:

  a. Fishing ground surveillance radar;

  b. Ground radar equipment specially designed for enroute air traffic control and having all the following:

   1. A maximum “instrumented range” of 500 km or less;

   2. Configured so that radar target data can be transmitted only one way from the radar site to one or more civil ATC centres;

   3. Contains no provisions for remote control of the radar scan rate from the enroute ATC centre; and

   4. Permanently installed;

  c. Weather balloon tracking radars.

 

 j. Being “laser” radar or Light Detection and Ranging (LIDAR) equipment and having any of the following:

 1. “Spacequalified”; or

 2. Employing coherent heterodyne or homodyne detection techniques and having an angular resolution of less (better) than 20 µrad (microradians);

 Note: 6A008.j. does not control LIDAR equipment specially designed for surveying or for meteorological observation.

 

 k. Having “signal processing” subsystems using “pulse compression” and having any of the following:

6A008 k. continued

 

 1. A “pulse compression” ratio exceeding 150; or

 2. A pulse width of less than 200 ns; or

 

 l. Having data processing subsystems and having any of the following:

 1. “Automatic target tracking” providing, at any antenna rotation, the predicted target position beyond the time of the next antenna beam passage;

 Note: 6A008.l.1. does not control conflict alert capability in ATC systems, or marine or harbour radar.

 2. Calculation of target velocity from primary radar having nonperiodic (variable) scanning rates;

 3. Processing for automatic pattern recognition (feature extraction) and comparison with target characteristic data bases (waveforms or imagery) to identify or classify targets; or

 4. Superposition and correlation, or fusion, of target data from two or more “geographically dispersed” and “interconnected radar sensors” to enhance and discriminate targets.

 Note: 6A008.l.4. does not control systems, equipment and assemblies used for marine traffic control.

 

 

6A102 Radiation hardened ‘detectors’, not controlled in 6A002, specially designed or modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), Xrays, combined blast and thermal effects) and usable for “missiles”, designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 x 105 rads (silicon).

 Technical Note:

 In 6A102, a ‘detector’ is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material.  This includes devices that sense by one time operation or failure.

 

 

6A107 Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows:

 

 a. Gravity meters, not controlled in 6A007.b, designed or modified for airborne or marine use, and having a static or operational accuracy of 7 x 106  m/s2 (0.7 milligal) or less (better), and having a timetosteadystate registration of two minutes or less;

 b. Specially designed components for gravity meters specified in 6A007.b or 6A107.a. and gravity gradiometers specified in 6A007.c.

 

 

6A108 Radar systems and tracking systems, not controlled in entry 6A008, as follows:

 

 a. Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

6A108 continued

 

 Note: 6A108.a. includes the following:

  a. Terrain contour mapping equipment;

  b. Imaging sensor equipment;

  c. Scene mapping and correlation (both digital and analogue) equipment;

d.        Doppler navigation radar equipment.

 

 b. Precision tracking systems, usable for ‘missiles’, as follows:

 1. Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide realtime measurements of inflight position and velocity;

 2. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:

 a. Angular resolution better than 3 milliradians;

 b. Range of 30 km or greater with a range resolution better than 10 m rms;

 c. Velocity resolution better than 3 m/s.

 Technical Note:

 In 6A108.b. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

6A202 Photomultiplier tubes having both of the following characteristics:

 

 a. Photocathode area of greater than 20 cm2; and

 

 b. Anode pulse rise time of less than 1 ns.

 

 

6A203 Cameras and components, not controlled in 6A003, as follows:

 

 a. Mechanical rotating mirror cameras, as follows, and specially designed components therefor:

 1. Framing cameras with recording rates greater than 225,000 frames per second;

 2. Streak cameras with writing speeds greater than 0.5 mm per microsecond;

 Note: In 6A203.a. components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors and bearings.

 

 b. Electronic streak cameras, electronic framing cameras, tubes and devices, as follows:

 1. Electronic streak cameras capable of 50 ns or less time resolution;

 2. Streak tubes for cameras specified in 6A203.b.1.;

 3. Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time;

 4. Framing tubes and solidstate imaging devices for use with cameras specified in 6A203.b.3., as follows:

 

6A203 b. continued

 

 a. Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance;

 b. Gate silicon intensifier target (SIT) videcon tubes, where a fast system allows gating the photoelectrons from the photocathode before they impinge on the SIT plate;

 c. Kerr or Pockels cell electrooptical shuttering;

 d. Other framing tubes and solidstate imaging devices having a fastimage gating time of less than 50 ns specially designed for cameras specified in 6A203.b.3.;

 

 c. Radiationhardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 50 x 103 Gy(silicon) (5 x 106 rad (silicon)) without operational degradation.

 Technical Note:

 The term Gy (silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation.

 

6A205 “Lasers”, “laser” amplifiers and oscillators, not controlled in 0B001.g.5., 0B001.h.6. and 6A005; as follows:

 N.B.: For copper vapour lasers, see 6A005.b.

 

 a. Argon ion “lasers” having both of the following characteristics:

 1. Operating at wavelengths between 400 nm and 515 nm; and

 2. An average output power greater than 40 W;

 

 b. Tunable pulsed singlemode dye laser oscillators having all of the following characteristics:

 1. Operating at wavelengths between 300 nm and 800 nm;

 2. An average output power greater than 1 W;

 3. A repetition rate greater than 1 kHz; and

 4. Pulse width less than 100 ns;

 

 c. Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:

 1. Operating at wavelengths between 300 nm and 800 nm;

 2. An average output power greater than 30 W;

 3. A repetition rate greater than 1 kHz; and

 4. Pulse width less than 100 ns;

 Note: 6A205.c. does not control single mode oscillators;

 

 d. Pulsed carbon dioxide “lasers” having all of the following characteristics:

 1. Operating at wavelengths between 9,000 nm and 11,000 nm;

 2. A repetition rate greater than 250 Hz;

 3. An average output power greater than 500 W; and

 4. Pulse width of less than 200 ns;

 

 

6A205 continued

 

 e. Parahydrogen Raman shifters designed to operate at 16 micrometre output wavelength and at a repetition rate greater than 250 Hz;

 

 f. Neodymiumdoped (other than glass) “lasers” with an output wavelength between 1000 and 1100 nm having either of the following:

 1. Pulseexcited and Qswitched with a pulse duration equal to or more than 1 ns and having either of the following:

 a. A single–transverse mode output with an average output power greater than 40W; or

 b. A multipletransverse mode output having an average power greater than 50 W;

  or

 2. Incorporating frequency doubling to give an output wavelength between 500 and 550 nm with an average output power of more than 40 W.

 

 

6A225 Velocity interferometers for measuring velocities exceeding 1 km/s during time

 intervals of less than 10 microseconds.

 Note: 6A225 includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).

 

 

6A226 Pressure sensors, as follows:

 

 a. Manganin gauges for pressures greater than 10 GPa;

 

 b. Quartz pressure transducers for pressures greater than 10 GPa.

 

 

6B Test, Inspection and Production Equipment

 

6B004 Optical equipment as follows:

 

 a. Equipment for measuring absolute reflectance to an accuracy of ± 0.1% of the reflectance value;

 

 b. Equipment other than optical surface scattering measurement equipment, having an unobscured aperture of more than 10 cm, specially designed for the noncontact optical measurement of a nonplanar optical surface figure (profile) to an “accuracy” of 2 nm or less (better) against the required profile.

 

 Note: 6B004 does not control microscopes.

 

 

6B007 Equipment to produce, align and calibrate landbased gravity meters with a static accuracy of better than 0.1 mgal.

 

6B008 Pulse radar crosssection measurement systems having transmit pulse widths of 100 ns or less and specially designed components therefor.

 N.B.: SEE ALSO 6B108.

 

 

6B108 Systems, not controlled in 6B008, specially designed for radar cross section measurement usable for ‘missiles’ and their subsystems.

Technical Note:

 In 6B108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

6C Materials

 

6C002 Optical sensor materials as follows:

 

 a. Elemental tellurium (Te) of purity levels of 99.9995% or more;

 

 b. Single crystals (including epitaxial wafers) of any of the following:

 1. Cadmium zinc telluride (CdZnTe), with zinc content of less than 6% by ‘mole fraction’;

 2. Cadmium telluride (CdTe) of any purity level; or

 3. Mercury cadmium telluride (HgCdTe) of any purity level.

 Technical Note:

 ‘Mole fraction’ is defined as the ratio of moles of ZnTe to the sum of moles of CdTe and ZnTe present in the crystal.

 

 

6C004 Optical materials as follows:

 

 a. Zinc selenide (ZnSe) and zinc sulphide (ZnS) “substrate blanks”, produced by the chemical vapour deposition process and having any of the following:

 1. A volume greater than 100 cm3; or

 2. A diameter greater than 80 mm and a thickness of 20 mm or more;

 

 b. Boules of any of the following electrooptic materials:

 1. Potassium titanyl arsenate (KTA);

 2. Silver gallium selenide (AgGaSe2 ); or

 3. Thallium arsenic selenide (Tl3AsSe3, also known as TAS);

 

 c. Nonlinear optical materials having all of the following:

 1. Third order susceptibility (chi 3) of 106 m2/V2 or more; and

 2. A response time of less than 1 ms;

 

 d. “Substrate blanks” of silicon carbide or beryllium beryllium (Be/Be) deposited materials exceeding 300 mm in diameter or major axis length;

 

 

 

6C004 continued

 

 e. Glass, including fused silica, phosphate glass, fluorophosphate glass, zirconium fluoride (ZrF4 ) and hafnium fluoride (HfF4 ) and having all of the following:

 1. A hydroxyl ion (OH) concentration of less than 5 ppm;

 2. Integrated metallic purity levels of less than 1 ppm; and

 3. High homogeneity (index of refraction variance) less than 5 x 106;

 

 f. Synthetically produced diamond material with an absorption of less than

  105 cm1 for wavelengths exceeding 200 nm but not exceeding 14,000 nm.

 

 

6C005 Synthetic crystalline “laser” host material in unfinished form as follows:

 

 a. Titanium doped sapphire;

 

 b. Alexandrite.

 

 

6D Software

 

6D001 “Software” specially designed for the “development” or “production” of equipment specified in 6A004, 6A005, 6A008 or 6B008.

 

 

6D002 “Software” specially designed for the “use” of equipment specified in 6A002.b., 6A008 or 6B008.

 

 

6D003 Other “software” as follows:

 

 a. “Software” as follows:

  1. “Software” specially designed for acoustic beam forming for the “real time processing” of acoustic data for passive reception using towed hydrophone arrays;

 2. “Source code” for the “real time processing” of acoustic data for passive reception using towed hydrophone arrays;

 3. “Software” specially designed for acoustic beam forming for “real time processing” of acoustic data for passive reception using bottom or bay cable systems;

 4. “Source code” for “real time processing” of acoustic data for passive reception using bottom or bay cable systems;

 

 b. “Software” as follows:

  1. “Software” specially designed for magnetic and electric field “compensation systems” for magnetic and electric field sensors designed to operate on mobile platforms;

 2. “Software” specially designed for magnetic and electric field anomaly detection on mobile platforms;

6D003 continued

 

 c. “Software” specially designed to correct motional influences of gravity  meters or gravity gradiometers;

 

 d. “Software” as follows:

  1. Air Traffic Control (ATC) “software” application “programs” hosted on general purpose computers located at Air Traffic Control centres and capable of any of the following:

 a. Processing and displaying more than 150 simultaneous “system tracks”; or

 b. Accepting radar target data from more than four primary radars;

 2. “Software” for the design or “production” of radomes and having all of the following:

 a. Specially designed to protect the “electronically steerable phased array antennae” specified in 6A008.e.; and

 b. Resulting in an antenna pattern having an ‘average side lobe level’ more than 40 dB below the peak of the main beam level.

 Technical Note:

 ‘Average side lobe level’ in 6D003.d.2.b. is measured over the entire array excluding the angular extent of the main beam and the first two side lobes on either side of the main beam.

 

 

6D102 “Software” specially designed or modified for the “use” of goods specified in 6A108.

 

 

6D103 “Software” which processes postflight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for ‘missiles’.

Technical Note:

  In 6D103 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

6E Technology

 

6E001 “Technology” according to the General Technology Note for the “development” of equipment, materials or “software” specified in 6A, 6B, 6C or 6D.

 

 

6E002 “Technology” according to the General Technology Note for the “production” of

 equipment or materials specified in 6A, 6B or 6C.

 

 

6E003 Other “technology” as follows:

 

 a. “Technology” as follows:

 

 

6E003 continued

 

  1. Optical surface coating and treatment “technology”, “required” to achieve uniformity of 99.5% or better for optical coatings 500 mm or more in diameter or major axis length and with a total loss (absorption and scatter) of less than 5 x 103;

 N.B.: See also 2E003.f.

 

 2. Optical fabrication “technology” using single point diamond turning techniques to produce surface finish accuracies of better than 10 nm rms on nonplanar surfaces exceeding 0.5 m2;

 

 b. “Technology” “required” for the “development”, “production” or “use” of specially designed diagnostic instruments or targets in test facilities for “SHPL” testing or testing or evaluation of materials irradiated by “SHPL” beams;

 

 

6E101 “Technology” according to the General Technology Note for the “use” of equipment or “software” specified in 6A002, 6A007.b. and c., 6A008, 6A102, 6A107, 6A108, 6B108, 6D102 or 6D103.

 Note: 6E101 only specifies “technology” for equipment specified in 6A008 when it is designed for airborne applications and is usable in “missiles”.

 

 

6E201 “Technology” according to the General Technology Note for the “use” of equipment specified in 6A003, 6A005.a.2., 6A005.b.2., 6A005.b.3., 6A005.b.4., 6A005.b.6., 6A005.c.2., 6A005.d.3.c., 6A005.d.4.c., 6A202, 6A203, 6A205, 6A225 or 6A226.

 

CATEGORY 7 NAVIGATION AND AVIONICS

 

 

 

7A Systems, Equipment and Components

 

 N.B.: For automatic pilots for underwater vehicles, see Category 8.

  For radar, see Category 6.

 

 

7A001 Accelerometers as follows and specially designed components therefor:

 N.B.: SEE ALSO 7A101.

 N.B.: For angular or rotational accelerometers, see 7A001.b.

 

 a. Linear accelerometers having any of the following:

1.  Specified to function at linear acceleration levels less than or equal to 15 g and having any of the following:

a.  A “bias” “stability” of less (better) than 130 micro g with respect to a fixed calibration value over a period of one year; or

b.  A “scale factor” “stability” of less (better) than 130 ppm with respect to a fixed calibration value over a period of one year;

2. Specified to function at linear acceleration levels exceeding 15 g and having all of the following:

 a. A “bias” “repeatability” of less (better) than 5,000 micro g over a period of one year; and

 b. A “scale factor” “repeatability” of less (better) than 2,500 ppm over a period of one year; or

3. Designed for use in inertial navigation or guidance systems and specified to function at linear acceleration levels exceeding 100 g;

 

 b. Angular or rotational accelerometers specified to function at linear acceleration levels exceeding 100 g.

 

 

7A002 Gyros, and angular rate sensors, having any of the following and specially designed components therefor:

 N.B.: SEE ALSO 7A102.

 N.B.: For angular or rotational accelerometers, see 7A001.b.  

 

a. A “bias” “stability”, when measured in a 1 g environment over a period of one month, and with respect to a fixed calibration value of less (better) than 0.5 degree per hour when specified to function at linear acceleration levels up to and including 100 g;

 

 b. An “angle random walk” of less (better) than or equal to 0.0035 degree per square root hour; or

 Note: 7A002.b. does not control spinning mass gyros’.

 

 

7A002 continued

 

 Technical Note:

 ‘Spinning mass gyros are gyros which use a continually rotating mass to sense angular motion.

 

 c. A rate range greater than or equal to 500 degrees per second and having any of the following:

 1. A “bias” “stability”, when measured in a 1 g environment over a period of three minutes, and with respect to a fixed calibration value of less (better) than 40 degrees per hour; or

 2. An “angle random walk” of less (better) than or equal to 0.2 degree per square root hour; or

 

 d. Specified to function at linear acceleration levels exceeding 100 g.

 

 

7A003 Inertial systems and specially designed components, as follows:

 N.B.: SEE ALSO 7A103.

 

 a. Inertial Navigation Systems (INS) (gimballed or strapdown) and inertial equipment, designed for “aircraft”, land vehicle, vessels (surface or underwater) or “spacecraft” for navigation, attitude, guidance or control and having any of the following and specially designed components therefor:

 1. Navigation error (free inertial) subsequent to normal alignment of 0.8 nautical mile per hour (nm/hr) ‘Circular Error Probable’ (‘CEP’) or less (better); or

 2. Specified to function at linear acceleration levels exceeding 10 g;

 

 b. Hybrid Inertial Navigation Systems embedded with Global Navigation Satellite Systems(s) (GNSS) or with “DataBased Referenced Navigation” (“DBRN”) System(s) for navigation, attitude, guidance or control, subsequent to normal alignment and having an INS navigation position accuracy, after loss of GNSS or “DBRN” for a period of up to four minutes, of less (better) than 10 metres ‘Circular Error Probable’ (‘CEP’);

 

 c. Inertial Measurement Equipment for heading, or True North determination and having any of the following and specially designed components therefor:

 1. Designed to have heading, or True North determination accuracy equal to or less (better) than 0.07 deg sec (Lat) equivalent to 6 arc minutes rms at 45 degrees latitude; or

 2. Designed to have a nonoperating shock level of 900 g or greater at a duration of 1 msec or greater;

 

d. Inertial measurement equipment including Inertial Measurement Units (IMU) and Inertial Reference Systems (IRS), incorporating accelerometers or gyros specified in 7A001 or 7A002, and specially designed components therefor.

 

 

7A003 d. continued

 

 Note 1: The parameters of 7A003.a. and 7A003.b. are applicable with any of the following environmental conditions:

 

  a.. Input random vibration with an overall magnitude of 7.7 g rms in the first 0.5 hour and a total test duration of 1.5 hour per axis in each of the 3 perpendicular axes, when the random vibration meets all  the following:

  1. A constant Power Spectral Density (PSD) value of 0.04 g2/Hz over a frequency interval of 15 to 1,000 Hz; and

  2. The PSD attenuates with frequency from 0.04 g2/Hz to 0.01 g2/Hz over a frequency interval from 1,000 to 2,000 Hz;

  b. An angular rate capability about one or more axes of equal to or more than +2.62 rad/s (150 deg/s); or

  c. According to national standards equivalent to a. or b. above.

 

 Note 2: 7A003 does not control inertial navigation systems which are certified for use on “civil aircraft” by civil authorities of a “participating state”.

 

 Note 3: 7A003.c.1. does not control theodolite systems incorporating inertial equipment specially designed for civil surveying purposes.

 

Technical Notes:

 

 1. 7A003.b. refers to systems in which an INS and other independent navigation aids are built into a single unit (embedded) in order to achieve improved performance.

 

 2. ‘Circular Error Probable’ (‘CEP’) – In a circular normal distribution, the radius of the circle containing 50 percent of the individual measurements being made, or the radius of the circle within which there is a 50 percent probability of being located.

 

 

7A004 Gyroastro compasses and other devices which derive position or orientation by means of automatically tracking celestial bodies or satellites, with an azimuth accuracy of equal to or less (better) than 5 seconds of arc.

 N.B.: SEE ALSO 7A104.

 

 

7A005 Global navigation satellite systems (i.e. GPS or GLONASS) receiving equipment having any of the following and specially designed components therefor:

 N.B.: SEE ALSO 7A105.

 

 a. Employing decryption; or

 

 b. Incorporating a nullsteerable antenna.

 

7A006 Airborne altimeters operating at frequencies other than 4.2 to 4.4 GHz inclusive and having any of the following:

 N.B.: SEE ALSO 7A106.

 

 a. “Power management”; or

 b. Using phase shift key modulation.

 

 

7A007 Deleted.

 

 

7A008 Underwater sonar navigation systems using dopplervelocity or correlation velocity logs integrated with a heading source and having a positioning accuracy of equal to or less (better) than 3% of distance travelled Circular Error Probable (CEP), and specially designed components therefor.

 

 Note: 7A008 does not control systems specially designed for installation on surface vessels or systems requiring acoustic beacons or buoys to provide positioning data.

 

 N.B.:  See 6A001.a. for acoustic systems, and 6A001.b. for correlationvelocity and Dopplervelocity sonar log equipment. 

  See 8A002 for other marine systems.

 

 

7A101 Accelerometers, not controlled in 7A001, as follows, and specially designed components therefor:

 

 a. Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in ‘missiles’, having all the following characteristics, and specially designed components therefor;

1. A “bias”  “repeatability” of less (better) than 1250 micro g; and

 

2. A “scale factor” “repeatability” of less (better) than 1250 ppm;

 Note: 7A101.a. does not specify accelerometers which are specially designed and developed as MWD (Measurement While Drilling) Sensors for use in downhole well service operations.

 

 Technical Notes:

1. In 7A101.a. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km;

2. In 7A101.a. the measurement of “bias” and “scale factor” refers to a one sigma standard deviation with respect to a fixed calibration over a period of one year.

 

 b. Continuous output accelerometers specified to function at acceleration levels exceeding 100g.

 

 

7A102 All types of gyros, not controlled in 7A002, usable in ‘missiles’, with a rated “drift rate” ‘stability’ of less than 0.5° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor.

 

Technical Notes:

1. In 7A102 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km;

2. In 7A102’stability’ is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition (IEEE STD 5282001 paragraph 2.247).

 

 

7A103 Instrumentation, navigation equipment and systems, not controlled in 7A003, as follows; and specially designed components therefor:

 

 a. Inertial or other equipment, using accelerometers or gyros as follows, and systems incorporating such equipment:

 1. Accelerometers specified in 7A001.a.3., 7A001.b. or 7A101 or gyros specified in 7A002 or 7A102; or

 2. Accelerometers specified in 7A001.a.1. or 7A001.a.2. and having all of the following:

 a. Designed for use in inertial navigation systems or in guidance systems of all types and usable in ‘missiles’;

 b. A “bias” “repeatability” of less (better) than 1250 micro g; and

 c. A “scale factor” “repeatability” of less (better) than 1250 ppm;

 

 Note: 7A103.a. does not specify equipment containing accelerometers specified in 7A001 where such accelerometers are specially designed and developed as MWD (Measurement While Drilling) sensors for use in downhole well services operations.

 

 b. Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in ‘missiles’;

 

 c. ‘Integrated navigation systems’, designed or modified for ‘missiles’ and capable of providing a navigational accuracy of 200 m ‘Circle of Equal Probability’ (‘CEP’) or less;

 

 Technical Note:

 An ‘integrated navigation system’ typically incorporates the following components:

1. An inertial measurement device (e.g., an attitude and heading reference system, inertial reference unit, or inertial navigation system);

2. One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g., satellite navigation receiver, radar altimeter, and/or Doppler radar); and

3. Integration hardware and software.

 

 

7A103 continued

 

d. Three axis magnetic heading sensors, designed or modified to be integrated with flight control and navigation systems, having all the following characteristics, and specially designed components therefor;

 1. Internal tilt compensation in pitch (± 90 degrees) and roll (± 180 degrees) axes; and             

2. Capable of providing azimuthal accuracy better (less) than 0.5 degrees rms at latitude of ± 80 degrees, reference to local magnetic field.

 Note: Flight control and navigation systems in 7A103.d. include gyrostabilizers, automatic pilots and inertial navigation systems.

 

Technical Note:

In 7A103 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

7A104 Gyroastro compasses and other devices, not controlled in 7A004, which derive position or orientation by means of automatically tracking celestial bodies or satellites and specially designed components therefor.

 

 

7A105 Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS,

 GLONASS, or Galileo), having any of the following characteristics, and specially designed components therefor:

 

 a. Designed or modified for use in space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012  or sounding rockets specified in 9A104; or

 

 b. Designed or modified for airborne applications and having any of the following:

 1. Capable of providing navigation information at speeds in excess of 600 m/s (1,165 nautical miles/hour);

 2. Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secured signal/data; or

 3. Being specially designed to employ antijam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures.

  Note: 7A105.b.2. and 7A105.b.3. do not control equipment designed for commercial, civil or ‘Safety of Life’ (e.g., data integrity, flight safety) GNSS services.

 

 

7A106 Altimeters, not controlled in 7A006, of radar or laser radar type, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

7A115 Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 Note: 7A115 includes sensors for the following equipment:

  a. Terrain contour mapping equipment;

  b. Imaging sensor equipment (both active and passive);

  c. Passive interferometer equipment.

 

 

7A116 Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 a. Hydraulic, mechanical, electrooptical, or electromechanical flight control systems (including flybywire types);

 

 b. Attitude control equipment;

 

 c. Flight control servo valves designed or modified for the systems specified in 7A116.a. or 7A116.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.

 

 

7A117 “Guidance sets”, usable in “missiles” capable of achieving system accuracy of 3.33% or less of the range (e.g., a “CEP” of 10 km or less at a range of 300 km).

 

 

7B Test, Inspection and Production Equipment

 

7B001 Test, calibration or alignment equipment, specially designed for equipment specified in 7A.

 

 Note: 7B001 does not control test, calibration or alignment equipment for Maintenance Level I or Maintenance Level II.

 

 Technical Notes:

 

 1. Maintenance Level I

  The failure of an inertial navigation unit is detected on the aircraft by indications from the Control and Display Unit (CDU) or by the status message from the corresponding subsystem. By following the manufacturer’s manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU).  The operator then removes the LRU and replaces it with a spare.

 

7B001 continued

 

 2. Maintenance Level II

  The defective LRU is sent to the maintenance workshop (the manufacturer’s or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer.

 N.B.: Maintenance Level II does not include the removal of controlled accelerometers or gyro sensors from the SRA.

 

 

7B002 Equipment specially designed to characterize mirrors for ring “laser” gyros, as follows:

 N.B.: SEE ALSO 7B102.

 

 a. Scatterometers having a measurement accuracy of 10 ppm or less (better);

 

 b. Profilometers having a measurement accuracy of 0.5 nm (5 angstrom) or less (better).

 

 

7B003 Equipment specially designed for the “production” of equipment specified in 7A.

 

 Note: 7B003 includes:

   Gyro tuning test stations;

   Gyro dynamic balance stations;

   Gyro runin/motor test stations;

   Gyro evacuation and fill stations;

   Centrifuge fixtures for gyro bearings;

   Accelerometer axis align stations;

   Fibre optic gyro coil winding machines.

 

 

7B102 Reflectometers specially designed to characterise mirrors, for “laser” gyros, having a measurement accuracy of 50 ppm or less (better).

 

 

7B103 “Production facilities” and “production equipment” as follows:

 

 a. “Production facilities” specially designed for equipment specified in 7A117;

 

 b. “Production equipment”, and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A.

 

7C Materials

 

 None.

 

7D Software

 

7D001 “Software” specially designed or modified for the “development” or “production” of equipment specified in 7A. or 7B.

 

 

7D002 “Source code” for the “use” of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems (‘AHRS’).

 

 Note: 7D002 does not control “source code” for the “use” of gimballed ‘AHRS’.

 

 Technical Note:

 ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.

 

 

7D003 Other “software” as follows:

 

 a. “Software” specially designed or modified to improve the operational performance or reduce the navigational error of systems to the levels specified in 7A003, 7A004 or 7A008;

 

 b. “Source code” for hybrid integrated systems which improves the operational performance or reduces the navigational error of systems to the level specified in 7A003 or 7A008 by continuously combining heading data with any of the following:

 1. Doppler radar or sonar velocity data;

 2. Global navigation satellite systems (i.e., GPS or GLONASS) reference data; or

 3. Data from “DataBased Referenced Navigation” (“DBRN”) systems;

 

 c. “Source code” for integrated avionics or mission systems which combine sensor data and employ “expert systems”;

 

 d. “Source code” for the “development” of any of the following:

 1. Digital flight management systems for “total control of flight”;

 2. Integrated propulsion and flight control systems;

 3. Flybywire or flybylight control systems;

 4. Faulttolerant or selfreconfiguring “active flight control systems”;

 5. Airborne automatic direction finding equipment;

 6. Air data systems based on surface static data; or

 7. Rastertype headup displays or three dimensional displays;

7D003 continued

 

 e. ComputerAidedDesign (CAD) “software” specially designed for the “development” of “active flight control systems”, helicopter multiaxis flybywire or flybylight controllers or helicopter “circulation controlled antitorque or circulationcontrolled direction control systems”, whose “technology” is specified in 7E004.b., 7E004.c.1. or 7E004.c.2.

 

 

7D101 “Software” specially designed or modified for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.

 

 

7D102 Integration “software” as follows:

 

 a. Integration “software” for the equipment specified in 7A103.b.;

 

 b. Integration “software” specially designed for the equipment specified in 7A003 or 7A103.a.;

 

 c. Integration “software” designed or modified for the equipment specified in 7A103.c.

 Note: A common form of integration “software” employs Kalman filtering.

 

 

7D103 “Software” specially designed for modelling or simulation of the “guidance sets”

 specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 Note: “Software” specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102.

 

 

7E Technology

 

7E001 “Technology” according to the General Technology Note for the “development” of equipment or “software”, specified in 7A, 7B or 7D.

 

 

7E002 “Technology” according to the General Technology Note for the “production” of

 equipment specified in 7A or 7B.

 

 

7E003 “Technology” according to the General Technology Note for the repair, refurbishing or overhaul of equipment specified in 7A001 to 7A004.

 

 Note: 7E003 does not control maintenance “technology” directly associated with calibration, removal or replacement of damaged or unserviceable LRUs and SRAs of a “civil aircraft” as described in ‘Maintenance Level I’ or ‘Maintenance Level II’.

  N.B.: See Technical Notes to 7B001.

 

7E004 Other “technology” as follows:

 

 a. “Technology” for the “development” or “production” of any of the following:

 1. Airborne automatic direction finding equipment operating at frequencies exceeding 5 MHz;

 2. Air data systems based on surface static data only, i.e., which dispense with conventional air data probes;

 3. Rastertype headup displays or three dimensional displays for “aircraft”;

 4. Inertial navigation systems or gyroastro compasses containing accelerometers or gyros specified in 7A001 or 7A002;

 5. Electric actuators (i.e., electromechanical, electrohydrostatic and integrated actuator package) specially designed for “primary flight control”;

 6. “Flight control optical sensor array” specially designed for implementing “active flight control systems”; or

 7. “DBRN” systems designed to navigate underwater, using sonar or gravity databases, that provide a positioning accuracy equal to or less (better) than 0.4 nautical miles;

 

 b. “Development” “technology”, as follows, for “active flight control systems” (including flybywire or flybylight):

 1. Configuration design for interconnecting multiple microelectronic processing elements (onboard computers) to achieve “real time processing” for control law implementation;

 2. Control law compensation for sensor location or dynamic airframe loads, i.e., compensation for sensor vibration environment or for variation of sensor location from the centre of gravity;

 3. Electronic management of data redundancy or systems redundancy for fault detection, fault tolerance, fault isolation or reconfiguration;

 Note:  7E004.b.3. does not control “technology” for the design of physical redundancy.

 4. Flight controls which permit inflight reconfiguration of force and moment controls for real time autonomous air vehicle control;

 5. Integration of digital flight control, navigation and propulsion control data into a digital flight management system for “total control of flight”;

 

 Note: 7E004.b.5. does not control:

  a. “Development” “technology” for integration of digital flight control, navigation and propulsion control data into a digital flight management system for “flight path optimisation”;

  b. “Development” “technology” for “aircraft” flight instrument systems integrated solely for VOR, DME, ILS or MLS navigation or approaches.

 6. Full authority digital flight control or multisensor mission management systems employing “expert systems”;

 

7E004 b. continued

 

 N.B.: For “technology” for Full Authority Digital Engine Control (“FADEC”), see 9E003.a.9.

 

 c. “Technology” for the “development” of helicopter systems, as follows:

 1. Multiaxis flybywire or flybylight controllers which combine the functions of at least two of the following into one controlling element:

 a. Collective controls;

 b. Cyclic controls;

 c. Yaw controls;

 2. “Circulationcontrolled antitorque or circulationcontrolled directional control systems”;

 3. Rotor blades incorporating “variable geometry airfoils” for use in systems using individual blade control.

 

 

7E101 “Technology” according to the General Technology Note for the “use” of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7B001, 7B002, 7B003, 7B102, 7B103, 7D101 to 7D103.

 

 

7E102 “Technology” for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows:

 

 a. Design “technology” for shielding systems;

 

 b. Design “technology” for the configuration of hardened electrical circuits and subsystems;

 c. Design “technology” for the determination of hardening criteria of 7E102.a. and 7E102.b.

 

 

7E104 “Technology” for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory.

 

CATEGORY 8 MARINE

 

 

 

8A Systems, Equipment and Components

 

8A001 Submersible vehicles and surface vessels, as follows:

 Note: For the control status of equipment for submersible vehicles, see:

   Category 5 – Part 2 “Information Security” for encrypted communication equipment;

     Category 6 for sensors;

     Categories 7 and 8 for navigation equipment;

     Category 8A for underwater equipment.

 

 a. Manned, tethered submersible vehicles designed to operate at depths exceeding 1,000 m;

 

 b. Manned, untethered submersible vehicles having any of the following:

 1. Designed to ‘operate autonomously’ and having a lifting capacity of all the following:

 a. 10% or more of their weight in air; and

 b. 15 kN or more;

 2. Designed to operate at depths exceeding 1,000 m; or

 3. Having all of the following:

 a. Designed to carry a crew of 4 or more;

 b. Designed to ‘operate autonomously’ for 10 hours or more;

 c. ‘Range’ of 25 nautical miles or more; and

 d. Length of 21 m or less;

 

 Technical Notes:

 1. For the purposes of 8A001.b., ‘operate autonomously’ means fully submerged, without snorkel, all systems working and cruising at minimum speed at which the submersible can safely control its depth dynamically by using its depth planes only, with no need for a support vessel or support base on the surface, seabed or shore, and containing a propulsion system for submerged or surface use.

 2. For the purposes of 8A001.b., ‘range’ means half the maximum distance a submersible vehicle can cover.

 

 c. Unmanned, tethered submersible vehicles designed to operate at depths exceeding 1,000 m and having any of the following:

 1. Designed for selfpropelled manoeuvre using propulsion motors or thrusters specified in  8A002.a.2.; or

 2. Fibre optic data link;

 

 d. Unmanned, untethered submersible vehicles having any of the following:

 1. Designed for deciding a course relative to any geographical reference without realtime human assistance;

 2. Acoustic data or command link; or

8A001 d. continued

 

 3. Fibre optic data or command link exceeding 1,000 m;

 

 e. Ocean salvage systems with a lifting capacity exceeding 5 MN for salvaging objects from depths exceeding 250 m and having any of the following:

 1. Dynamic positioning systems capable of position keeping within 20 m of a given point provided by the navigation system; or

 2. Seafloor navigation and navigation integration systems for depths exceeding 1,000 m and with positioning accuracies to within 10 m of a predetermined point;

 

 f. Surfaceeffect vehicles (fully skirted variety) having all of the following:

 1. Maximum design speed, fully loaded, exceeding 30 knots in a significant wave height of 1.25 m (Sea State 3) or more;

 2. Cushion pressure exceeding 3,830 Pa; and

 3. Lightshiptofullload displacement ratio of less than 0.70;

 

 g. Surfaceeffect vehicles (rigid sidewalls) with a maximum design speed, fully loaded, exceeding 40 knots in a significant wave height of 3.25 m (Sea State 5) or more;

 

 h. Hydrofoil vessels with active systems for automatically controlling foil systems, with a maximum design speed, fully loaded, of 40 knots or more in a significant wave height of 3.25 m (Sea State 5) or more;

 

 i. ‘Small waterplane area vessels’ having any of the following:

 1. Full load displacement exceeding 500 tonnes with a maximum design speed, fully loaded, exceeding 35 knots in a significant wave height of 3.25 m (Sea State 5) or more; or

 2. Full load displacement exceeding 1,500 tonnes with a maximum design speed, fully loaded, exceeding 25 knots in a significant wave height of 4 m (Sea State 6) or more.

 Technical Note:

 A ‘small waterplane area vessel’ is defined by the following formula: waterplane area at an operational design draught less than 2 x (displaced volume at the operational design draught)2/3.

 

 

8A002 Marine systems, equipment and components, as follows:

 

 Note: For underwater communications systems, see Category 5 – Part 1 Telecommunications.

 

 a. Systems equipment and components, specially designed or modified for submersible vehicles and designed to operate at depths exceeding 1,000 m, as follows:

 1. Pressure housings or pressure hulls with a maximum inside chamber diameter exceeding 1.5 m;

 

8A002 a. continued

 

 2. Direct current propulsion motors or thrusters;

 3. Umbilical cables, and connectors therefor, using optical fibre and having synthetic strength members;

 4. Components manufactured from material specified in 8C001;

Technical Note:

The objective of 8A002.a.4. should not be defeated by the export of syntactic foam specified in 8C001 when an intermediate stage of manufacture has been performed and it is not yet in the final component form.

 

 b. Systems specially designed or modified for the automated control of the motion of submersible vehicles specified in 8A001 using navigation data, having closed loop servocontrols and having any of the following:

 1. Enabling a vehicle to move within 10 m of a predetermined point in the water column;

 2. Maintaining the position of the vehicle within 10 m of a predetermined point in the water column; or

 3. Maintaining the position of the vehicle within 10 m while following a cable on or under the seabed;

 

 c. Fibre optic hull penetrators or connectors;

 

 d. Underwater vision systems as follows:

 1. Television systems and television cameras, as follows:

 a. Television systems (comprising camera, monitoring and signal transmission equipment) having a ‘limiting resolution’ when measured in air of more than 800 lines and specially designed or modified for remote operation with a submersible vehicle;

 b. Underwater television cameras having a ‘limiting resolution’ when measured in air of more than 1,100 lines;

 c. Low light level television cameras specially designed or modified for underwater use and having all of the following:

 1. Image intensifier tubes specified in 6A002.a.2.a.; and

 2. More than 150,000 “active pixels” per solid state area array;

 Technical Note:

 ‘Limiting resolution’ is a measure of horizontal resolution usually expressed in terms of the maximum number of lines per picture height discriminated on a test chart, using IEEE Standard 208/1960 or any equivalent standard.

 2. Systems specially designed or modified for remote operation with an underwater vehicle, employing techniques to minimise the effects of back scatter and including rangegated illuminators or “laser” systems;

 

 e. Photographic still cameras specially designed or modified for underwater use below 150 m, with a film format of 35 mm or larger and having any of the following:

8A002 e. continued

 

 1. Annotation of the film with data provided by a source external to the camera;

 2. Automatic back focal distance correction; or

 3. Automatic compensation control specially designed to permit an underwater camera housing to be usable at depths exceeding 1,000 m;

 

 f. Electronic imaging systems, specially designed or modified for underwater use, capable of storing digitally more than 50 exposed images;

 Note: 8A002.f. does not control digital cameras specially designed for consumer purposes, other than those employing electronic image multiplication techniques.

 

 g. Light systems specially designed or modified for underwater use, as follows:

 1. Stroboscopic light systems capable of a light output energy of more than 300 J per flash and a flash rate of more than 5 flashes per second;

 2. Argon arc light systems specially designed for use below 1,000 m;

 

 h. “Robots” specially designed for underwater use, controlled by using a dedicated computer and having any of the following:

 1. Systems that control the “robot” using information from sensors which measure force or torque applied to an external object, distance to an external object, or tactile sense between the “robot” and an external object; or

 2. The ability to exert a force of 250 N or more or a torque of 250 Nm or more and using titanium based alloys or “composite” “fibrous or filamentary” materials in their structural members;

 

 i. Remotely controlled articulated manipulators specially designed or modified for use with submersible vehicles and having any of the following:

 1. Systems which control the manipulator using the information from sensors which measure the torque or force applied to an external object, or tactile sense between the manipulator and an external object; or

 2. Controlled by proportional masterslave techniques or by using a dedicated computer and having 5 degrees of ‘freedom of movement’ or more;

 Technical Note: 

 Only functions having proportional control using positional feedback or by using a dedicated computer are counted when determining the number of degrees of freedom of movement.

 

 j. Air independent power systems specially designed for underwater use, as follows:

 1. Brayton or Rankine cycle engine air independent power systems having any of the following:

 

 

8A002 j. continued

 a. Chemical scrubber or absorber systems specially designed to remove carbon dioxide, carbon monoxide and particulates from recirculated engine exhaust;

 b. Systems specially designed to use a monoatomic gas;

 c. Devices or enclosures specially designed for underwater noise reduction in frequencies below 10 kHz, or special mounting devices for shock mitigation; or

 d. Systems having all of the following:

 1. Specially designed to pressurize the products of reaction or for fuel reformation;

 2. Specially designed to store the products of the reaction; and

 3. Specially designed to discharge the products of the reaction against a pressure of 100 kPa or more;

 2. Diesel cycle engine air independent systems having all of the following:

 a. Chemical scrubber or absorber systems specially designed to remove carbon dioxide, carbon monoxide and particulates from recirculated engine exhaust;

 b. Systems specially designed to use a monoatomic gas;

 c. Devices or enclosures specially designed for underwater noise reduction in frequencies below 10 kHz or special mounting devices for shock mitigation; and

 d. Specially designed exhaust systems that do not exhaust continuously the products of combustion;

 3. Fuel cell air independent power systems with an output exceeding 2 kW and having any of the following:

 a. Devices or enclosures specially designed for underwater noise reduction in frequencies below 10 kHz or special mounting devices for shock mitigation; or

 b. Systems having all of the following:

 1. Specially designed to pressurize the products of reaction or for fuel reformation;

 2. Specially designed to store the products of the reaction; and

 3. Specially designed to discharge the products of the reaction against a pressure of 100 kPa or more;

 4. Stirling cycle engine air independent power systems having all of the following:

 a. Devices or enclosures specially designed for underwater noise reduction in frequencies below 10 kHz or special mounting devices for shock mitigation; and

 b. Specially designed exhaust systems which discharge the products of combustion against a pressure of 100 kPa or more;

 

 k. Skirts, seals and fingers, having any of the following:

 1. Designed for cushion pressures of 3,830 Pa or more, operating in a significant wave height of 1.25 m (Sea State 3) or more and specially designed for surface effect vehicles (fully skirted variety) specified in  8A001.f.; or

8A002 k. continued

 

 2. Designed for cushion pressures of 6,224 Pa or more, operating in a significant wave height of 3.25 m (Sea State 5) or more and specially designed for surface effect vehicles (rigid sidewalls) specified in  8A001.g.;

 

 l. Lift fans rated at more than 400 kW and specially designed for surface effect vehicles specified in 8A001.f. or 8A001.g.;

 

 m. Fully submerged subcavitating or supercavitating hydrofoils specially designed for vessels specified in 8A001.h.;

 

 n. Active systems specially designed or modified to control automatically the seainduced motion of vehicles or vessels specified in 8A001.f., 8A001.g., 8A001.h. or 8A001.i.;

 

 o. Propellers, power transmission systems, power generation systems and noise reduction systems, as follows:

 1. Waterscrew propeller or power transmission systems, as follows, specially designed for surface effect vehicles (fully skirted or rigid sidewall variety), hydrofoils or ‘small waterplane area vessels’ specified in 8A001.f., 8A001.g., 8A001.h. or 8A001.i., as follows:

 a. Supercavitating, superventilated, partiallysubmerged or surface piercing propellers rated at more than 7.5 MW;

 b. Contrarotating propeller systems rated at more than 15 MW;

 c. Systems employing preswirl or postswirl techniques for smoothing the flow into a propeller;

 d. Lightweight, high capacity (K factor exceeding 300) reduction gearing;

 e. Power transmission shaft systems, incorporating “composite” material components and capable of transmitting more than 1 MW;

 2. Waterscrew propeller power generation systems or transmission systems designed for use on vessels, as follows:

 a. Controllablepitch propellers and hub assemblies rated at more than 30 MW;

 b. Internally liquidcooled electric propulsion engines with a power output exceeding 2.5 MW;

 c. “Superconductive” propulsion engines or permanent magnet electric propulsion engines, with a power output exceeding 0.1 MW;

 d. Power transmission shaft systems incorporating “composite” material components and capable of transmitting more than 2 MW;

 e. Ventilated or baseventilated propeller systems, rated at more than 2.5 MW;

 3. Noise reduction systems designed for use on vessels of 1,000 tonnes displacement or more, as follows:

 

 

8A002 o. continued

 

 a. Systems that attenuate underwater noise at frequencies below 500 Hz and consist of compound acoustic mounts for the acoustic

  isolation of diesel engines, diesel generator sets, gas turbines, gas turbine generator sets, propulsion motors or propulsion reduction gears, specially designed for sound or vibration isolation and having an intermediate mass exceeding 30% of the equipment to be mounted;

 b. Active noise reduction or cancellation systems, or magnetic bearings, specially designed for power transmission systems, and incorporating electronic control systems capable of actively reducing equipment vibration by the generation of antinoise or antivibration signals directly to the source;

 

 p. Pumpjet propulsion systems having a power output exceeding 2.5 MW using divergent nozzle and flow conditioning vane techniques to improve propulsive efficiency or reduce propulsiongenerated underwaterradiated noise;

 

 q. Selfcontained, closed or semiclosed circuit (rebreathing) diving and underwater swimming apparatus.

 Note: 8A002.q. does not control an individual apparatus for personal use when accompanying its user.

 

 

8B Test, Inspection and Production Equipment

 

8B001 Water tunnels having a background noise of less than 100 dB (reference 1 µPa, 1 Hz) in the frequency range from 0 to 500 Hz and designed for measuring acoustic fields generated by a hydroflow around propulsion system models.

 

 

8C Materials

 

8C001 ‘Syntactic foam’ designed for underwater use and having all of the following:

N.B.: SEE ALSO 8A002.a.4.

 

 a. Designed for marine depths exceeding 1,000 m; and

 

 b. A density less than 561 kg/m3.

 

 Technical Note:

 ‘Syntactic foam’ consists of hollow spheres of plastic or glass embedded in a resin matrix.

 

 


8D Software

 

 

8D001 “Software” specially designed or modified for the “development”, “production” or “use” of equipment or materials specified in  8A, 8B or 8C.

 

 

8D002 Specific “software” specially designed or modified for the “development”, “production”, repair, overhaul or refurbishing (remachining) of propellers specially designed for underwater noise reduction.

 

 

8E Technology

 

8E001 “Technology” according to the General Technology Note for the “development” or “production” of equipment or materials specified in  8A, 8B or 8C.

 

 

8E002 Other “technology” as follows:

 

 a. “Technology” for the “development”, “production”, repair, overhaul or refurbishing (remachining) of propellers specially designed for underwater noise reduction;

 

 b. “Technology” for the overhaul or refurbishing of equipment specified in 8A001, 8A002.b., 8A002.j., 8A002.o. or 8A002.p.

 

CATEGORY 9 – AEROSPACE AND PROPULSION

 

 

 

9A Systems, Equipment and Components

 

 N.B.: For propulsion systems designed or rated against neutron or transient ionizing radiation, see ML12.

 

 

9A001 Aero gas turbine engines having any of the following:

 N.B.: SEE ALSO 9A101.

 

 a. Incorporating any of the “technologies” specified in 9E003.a.; or

 Note: 9A001.a. does not control aero gas turbine engines which meet all of the following:

  a. Certified by the civil aviation authority in a “participating state”; and

  b. Intended to power nonmilitary manned aircraft for which any of the following has been issued by a “participating state” for the aircraft with this specific engine type:

1. A civil type certificate; or

2. An equivalent document recognized by the International Civil Aviation Organisation (ICAO).

 b. Designed to power an aircraft to cruise at Mach 1 or higher for more than thirty minutes.

 

 

9A002 ‘Marine gas turbine engines’ with an ISO standard continuous power rating of 24,245 kW or more and a specific fuel consumption not exceeding 0.219 kg/kWh in the power range from 35 to 100%, and specially designed assemblies and components therefor.

 

 Note: The term ‘marine gas turbine engines’ includes those industrial, or aeroderivative, gas turbine engines adapted for a ship’s electric power generation or propulsion.

 

 

9A003 Specially designed assemblies and components, incorporating any of the “technologies” specified in 9E003.a., for gas turbine engine propulsion systems and having any of the following:

 

 a. Specified in 9A001; or

 

 b. Whose design or production origins are either non“participating states” or unknown to the manufacturer.

 

 

 

9A004 Space launch vehicles and “spacecraft”.

 N.B.: SEE ALSO 9A104.

 

 Note: 9A004 does not control payloads.

 

  N.B.: For the control status of products contained in “spacecraft” payloads, see the appropriate Categories.

 

 

9A005 Liquid rocket propulsion systems containing any of the systems or components

 specified in 9A006.

 N.B.: SEE ALSO 9A105 AND 9A119.

 

 

9A006 Systems and components specially designed for liquid rocket propulsion systems, as follows:

 N.B.: SEE ALSO 9A106, 9A108 AND 9A120.

 

 a. Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30% per year;

 

 b. Cryogenic containers or closedcycle refrigeration systems capable of providing temperatures of 100 K (173°C) or less for “aircraft” capable of sustained flight at speeds exceeding Mach 3, launch vehicles or “spacecraft”;

 

 c. Slush hydrogen storage or transfer systems;

 

 d. High pressure (exceeding 17.5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems;

 

 e. Highpressure (exceeding 10.6 MPa) thrust chambers and nozzles therefor;

 

 f. Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders);

 

 g. Liquid propellant injectors with individual orifices of 0.381 mm or smaller in diameter (an area of 1.14 x 103 cm2 or smaller for noncircular orifices) and specially designed for liquid rocket engines;

 

 h. Onepiece carboncarbon thrust chambers or onepiece carboncarbon exit cones with densities exceeding 1.4 g/cm3 and tensile strengths exceeding 48 MPa.

 

 

9A007 Solid rocket propulsion systems having any of the following:

 N.B.: SEE ALSO 9A107 AND 9A119.

 

 a. Total impulse capacity exceeding 1.1 MNs;

 

 b. Specific impulse of 2.4 kNs/kg or more when the nozzle flow is expanded to ambient sea level conditions for an adjusted chamber pressure of 7 MPa;

 

 c. Stage mass fractions exceeding 88% and propellant solid loadings exceeding 86%;

 

 d. Components specified in 9A008; or

 

 e. Insulation and propellant bonding systems using directbonded motor designs to provide a ‘strong mechanical bond’ or a barrier to chemical migration between the solid propellant and case insulation material.

 Technical Note:

 ‘Strong mechanical bond’ means bond strength equal to or more than propellant strength.

 

 

9A008 Components specially designed for solid rocket propulsion systems, as follows:

 N.B.: SEE ALSO 9A108.

 

 a. Insulation and propellant bonding systems using liners to provide a ‘strong mechanical bond’ or a barrier to chemical migration between the solid propellant and case insulation material;

 Technical Note:

 ‘Strong mechanical bond’ means bond strength equal to or more than propellant strength.

 

 b. Filamentwound “composite” motor cases exceeding 0.61 m in diameter or having ‘structural efficiency ratios (PV/W)’ exceeding 25 km;

 Technical Note:

 ‘Structural efficiency ratio (PV/W)’ is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W).

 

 c. Nozzles with thrust levels exceeding 45 kN or nozzle throat erosion rates of less than 0.075 mm/s;

 

 d. Movable nozzle or secondary fluid injection thrust vector control systems capable of any of the following:

 1. Omniaxial movement exceeding ± 5°;

 2. Angular vector rotations of 20°/s or more; or

 3. Angular vector accelerations of 40°/s2 or more.

 

 

9A009 Hybrid rocket propulsion systems having any of the following:

 N.B.: SEE ALSO 9A109 AND 9A119.

 

 a. Total impulse capacity exceeding 1.1 MNs; or

 

 b. Thrust levels exceeding 220 kN in vacuum exit conditions.

 

 

9A010 Specially designed components, systems and structures for launch vehicles, launch vehicle propulsion systems or “spacecraft”, as follows:

 N.B.: SEE ALSO 1A002 AND 9A110.

 

 a. Components and structures each exceeding 10 kg and specially designed for launch vehicles manufactured using metal “matrix” “composite”, organic “composite”, ceramic “matrix” or intermetallic reinforced materials specified in 1C007 or 1C010;

 Note: The weight cutoff is not relevant for nose cones.

 

 b. Components and structures specially designed for launch vehicle propulsion systems specified in 9A005 to 9A009 manufactured using metal matrix, composite, organic composite, ceramic matrix or intermetallic reinforced materials specified in 1C007 or 1C010;

 

 c. Structural components and isolation systems specially designed to control actively the dynamic response or distortion of “spacecraft” structures;

 

 d. Pulsed liquid rocket engines with thrusttoweight ratios equal to or more than 1 kN/kg and a response time (the time required to achieve 90% of total rated thrust from startup)  of less than 30 ms.

 

 

9A011 Ramjet, scramjet or combined cycle engines and specially designed components therefor.

 N.B.: SEE ALSO 9A111 AND 9A118.

 

 

9A012 “Unmanned aerial vehicles” (“UAVs”), associated systems, equipment and components as follows:

 a. “UAVs” having any of the following:

 1. An autonomous flight control and navigation capability (e.g., an autopilot with an Inertial Navigation System); or

 2. Capability of controlledflight out of the direct vision range involving a human operator (e.g., televisual remote control);

 b. Associated systems, equipment and components as follows:

 1. Equipment specially designed for remotely controlling the “UAVs” specified in 9A012.a.;

 2. Guidance or control systems other than those specified in 7A and specially designed for integration into “UAVs” specified in 9A012.a.;

 3. Equipment and components specially designed to convert a manned “aircraft” to a “UAV” specified in 9A012.a.

9A012 b.continued

 

 4. Air breathing reciprocating or rotary internal combustion type engines, specially designed or modified to propel “UAVs” at altitudes above 50,000 feet (15,240 metres).

 

 

9A101 Lightweight turbojet and turbofan engines (including turbocompound engines), not controlled in 9A001, as follows:

 

 a. Engines having both of the following characteristics:

 1. Maximum thrust value greater than 400 N (achieved uninstalled) excluding civil certified engines with a maximum thrust value greater than 8,890 N (achieved uninstalled); and

 2. Specific fuel consumption of 0.15 kg/N/hr or less (at maximum continuous power at sea level static and standard conditions);

 

 b. Engines designed or modified for use in “missiles” or unmanned aerial vehicles specified in 9A012.

 

 

9A102 ‘Turboprop engine systems’ specially designed for unmanned aerial vehicles specified in

 9A012, and specially designed components therefor, having a ‘maximum power’ greater than 10 kW.

 

 Note: 9A102 does not control civil certified engines.

 

 Technical Notes:

 1. For the purposes of 9A102 a ‘turboprop engine system’ incorporates all of the following:

 a. Turboshaft engine; and

 b. Power transmission system to transfer the power to a propeller.

 2. For the purposes of 9A102 the ‘maximum power’ is achieved uninstalled at sea level standard conditions.

 

 

9A104 Sounding rockets, capable of a range of at least 300 km.

 N.B.: SEE ALSO 9A004.

 

 

9A105 Liquid propellant rocket engines, as follows:

 N.B.: SEE ALSO 9A119.

 

 a. Liquid propellant rocket engines usable in “missiles”, not controlled in 9A005, having a total impulse capacity equal to or greater than 1.1 MNs;

 

 b. Liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, not controlled in 9A005 or 9A105.a., having a total impulse capacity equal to or greater than of 0.841 MNs.

 

9A106 Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems:

 

 a. Ablative liners for thrust or combustion chambers, usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

 

 b. Rocket nozzles, usable in “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

 

 c. Thrust vector control subsystems usable in “missiles”;

 Technical Note:

 Examples of methods of achieving thrust vector control specified in 9A106.c. are:

 1. Flexible nozzle;

 2. Fluid or secondary gas injection;

 3. Movable engine or nozzle;

 4. Deflection of exhaust gas stream (jet vanes or probes); or

 5. Thrust tabs.

 

 d. Liquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, usable in “missiles”, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.

 Note: The only servo valves and pumps specified in 9A106.d., are the following:

  a. Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms;

  b. Pumps, for liquid propellants, with shaft speeds equal to or greater than 8,000 r.p.m. or with discharge pressures equal to or greater than 7 MPa.

 

 

9A107 Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, not controlled in 9A007, having total impulse capacity equal to or greater than 0.841 MNs.

 N.B.: SEE ALSO 9A119.

 

 

9A108 Components, other than those specified in 9A008, usable in “missiles”, as follows, specially designed for solid rocket propulsion systems:

 

 a. Rocket motor cases and “insulation” components therefor;

 

 b. Rocket nozzles;

 

 c. Thrust vector control subsystems.

 

9A108 continued

 

 Technical Note:

 Examples of methods of achieving thrust vector control specified in 9A108.c. are:

 1. Flexible nozzle;

 2. Fluid or secondary gas injection;

 3. Movable engine or nozzle;

 4. Deflection of exhaust gas stream (jet vanes or probes); or

 5. Thrust tabs.

 

 

9A109 Hybrid rocket motors, usable in ‘missiles’, other than those specified in 9A009, and specially designed components therefor.

 N.B.: SEE ALSO 9A119.

 Technical Note:

 In 9A109 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

9A110 Composite structures, laminates and manufactures thereof, not controlled in 9A010, specially designed for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 or the subsystems specified in 9A005, 9A007, 9A105.a., 9A106 to 9A108, 9A116 or 9A119.

 N.B.: SEE ALSO 1A002.

 

 

9A111 Pulse jet engines, usable in “missiles” or unmanned aerial vehicles specified in 9A012, and specially designed components therefor.

 N.B.: SEE ALSO 9A011 AND 9A118.

 

 

9A115 Launch support equipment as follows:

 

 a. Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104;

 

 b. Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

9A116 Reentry vehicles, usable in “missiles”, and equipment designed or modified therefor, as follows:

 

 a. Reentry vehicles;

 

 b. Heat shields and components therefor fabricated of ceramic or ablative materials;

9A116 continued

 

 c. Heat sinks and components therefor fabricated of lightweight, high heat capacity materials;

 

 d. Electronic equipment specially designed for reentry vehicles.

 

 

9A117 Staging mechanisms, separation mechanisms, and interstages, usable in “missiles”.

 

 

9A118 Devices to regulate combustion usable in engines, which are usable in “missiles” or unmanned aerial vehicles specified in 9A012, specified in 9A011 or 9A111.

 

 

9A119 Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.

 

 

9A120 Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or ‘other liquid propellants’, used in rocket systems capable of delivering at least a 500 kg payload to a range of at least

300 km.

 

 Note: In 9A120 ‘other liquid propellants’ includes, but is not limited to, propellants specified in ML8.b.

 

 

9A350 Spraying or fogging systems, specially designed or modified for fitting to aircraft, “lighterthanair vehicles” or unmanned aerial vehicles, and specially designed components therefor, as follows:

 

 a. Complete spraying or fogging systems capable of delivering, from a liquid suspension, an initial droplet ‘VMD’ of less than 50 µm at a flow rate of greater than two litres per minute;

 

 b. Spray booms or arrays of aerosol generating units capable of delivering, from a liquid suspension, an initial droplet ‘VMD’ of less than 50 µm at a flow rate of greater than two litres per minute;

 

 c. Aerosol generating units specially designed for fitting to systems specified in 9A350.a. and b.

 Note:  Aerosol generating units are devices specially designed or modified for fitting to aircraft such as nozzles, rotary drum atomizers and similar devices.

 

 Note: 9A350 does not control spraying or fogging systems and components that are demonstrated not to be capable of delivering biological agents in the form of infectious aerosols.

9A350 continued

 

 Technical Notes:

 1. Droplet size for spray equipment or nozzles specially designed for use on aircraft, “lighterthanair vehicles” or unmanned aerial vehicles should be measured using either of the following:

 a. Doppler laser method;

b.         Forward laser diffraction method.

 2. In 9A350 ‘VMD’ means Volume Median Diameter and for waterbased systems this equates to Mass Median Diameter (MMD).

 

 

9B Test, Inspection and Production Equipment

 

9B001 Equipment, tooling and fixtures, specially designed for manufacturing gas turbine blades, vanes or tip shroud castings, as follows:

 

 a. Directional solidification or single crystal casting equipment;

 

 b. Ceramic cores or shells;

 

 

9B002 Online (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for the “development” of gas turbine engines, assemblies or components and incorporating “technologies” specified in 9E003.a.

 

 

9B003 Equipment specially designed for the “production” or test of gas turbine brush seals

 designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500°C), and specially designed components or accessories therefor.

 

 

9B004 Tools, dies or fixtures for the solid state joining of “superalloy”, titanium or

 intermetallic airfoiltodisk combinations described in 9E003.a.3. or 9E003.a.6. for gas turbines.

 

 

9B005 Online (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following:

 N.B.: SEE ALSO 9B105.

 

 a. Wind tunnels designed for speeds of Mach 1.2 or more;

 Note: 9B005.a. does not control wind tunnels specially designed for educational purposes and having a ‘test section size’ (measured laterally) of less than 250 mm.

 Technical Note:

 ‘Test section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, at the largest test section location.

9B005 continued

 

 b. Devices for simulating flowenvironments at speeds exceeding Mach 5, including hotshot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns; or

 

 c. Wind tunnels or devices, other than twodimensional sections, capable of simulating Reynolds number flows exceeding 25 x 106.

 

 

9B006 Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1,273 K (1,000°C), and specially designed quartz heaters therefor.

 N.B.: SEE ALSO 9B106.

 

 

9B007 Equipment specially designed for inspecting the integrity of rocket motors and using NonDestructive Test (NDT) techniques other than planar xray or basic physical or chemical analysis.

 

 

9B008 Transducers specially designed for the direct measurement of the wall skin friction of the test flow with a stagnation temperature exceeding 833 K (560°C).

 

 

9B009 Tooling specially designed for producing turbine engine powder metallurgy rotor

 components capable of operating at stress levels of 60% of Ultimate Tensile Strength (UTS) or more and metal temperatures of 873 K (600°C) or more.

 

 

9B010 Equipment specially designed for the production of “UAVs” and associated systems, equipment and components specified in 9A012.

 

 

9B105 Wind tunnels for speeds of Mach 0.9 or more, usable for ‘missiles’ and their

 subsystems.

 N.B.: SEE ALSO 9B005.

Technical Note:

In 9B105 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

9B106 Environmental chambers and anechoic chambers, as follows:

 

 a. Environmental chambers capable of simulating all the following flight conditions:

 1. Having any of the following:

 a. Altitude equal to or greater than 15 km; or

9B106 a. continued

 

 b. Temperature range from below 223 K (50oC) to above 398 K (+125oC);

 

 2. Incorporating, or ‘designed or modified’ to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured ‘bare table’, between 20 Hz and 2 kHz imparting forces equal to or greater than 5 kN;

 

 Technical Notes:

1. 9B106.a.2. describes systems that are capable of generating a vibration environment with a single wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum).

2. In 9B106.a.2., ‘designed or modified’ means the environmental chamber provides appropriate interfaces (e.g., sealing devices) to incorporate a shaker unit or other vibration test equipment as specified in 2B116.

3. In 9B106.a.2. ‘bare table’ means a flat table, or surface with no fixture or fittings.

 

 b. Environmental chambers capable of simulating the following flight conditions:

 1. Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 µPa) or with a total rated acoustic power output of 4 kW or greater; and

 2. Altitude equal to or greater than 15 km; or

 3. Temperature range from below 223 K (50oC) to above 398 K

  (+125oC).

 

 

9B115 Specially designed “production equipment” for the systems, subsystems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.

 

 

9B116 Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, subsystems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A104 to 9A109, 9A111, or 9A116 to 9A119.

 

 

9B117 Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:

 

 a. The capacity to handle more than 68 kN of thrust; or

 

 b. Capable of simultaneously measuring the three axial thrust components.

 

 

9C Materials

 

9C108 “Insulation” material in bulk form and “interior lining”, not controlled in 9A008, for rocket motor cases usable in “missiles” or specially designed for ‘missiles’.

Technical Note:

In 9C108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

 

9C110 Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a “specific tensile strength” greater than 7.62 x 104 m and a “specific modulus” greater than 3.18 x 106 m.

 N.B.: SEE ALSO 1C010 AND 1C210.

 

 Note: The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (Tg), after cure, exceeding 418 K (145oC) as determined by ASTM D4065 or equivalent.

 

 

9D Software

 

9D001 “Software” specially designed or modified for the “development” of equipment or “technology” specified in 9A001 to 9A119, 9B or 9E003.

 

 

9D002 “Software” specially designed or modified for the “production” of equipment specified in 9A001 to 9A119 or 9B.

 

 

9D003 “Software” specially designed or modified for the “use” of “Full Authority Digital Electronic Engine Controls” (“FADEC”) for propulsion systems specified in 9A or equipment specified in 9B, as follows:

 

 a. “Software” in digital electronic controls for propulsion systems, aerospace test facilities or air breathing aeroengine test facilities;

 

 b. Faulttolerant “software” used in “FADEC” systems for propulsion systems and associated test facilities.

 

 

9D004 Other “software” as follows:

 

 a. 2D or 3D viscous “software” validated with wind tunnel or flight test data required for detailed engine flow modelling;

 

 b. “Software” for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress;

9D004 continued

 

 c. “Software” specially designed to control directional solidification or single crystal casting;

 

 d. “Software” in “source code”, “object code” or machine code required for the “use” of active compensating systems for rotor blade tip clearance control;

 Note: 9D004.d. does not control “software” embedded in equipment not specified in Annex I or required for maintenance activities associated with the calibration or repair or updates to the active compensating clearance control system.

 e. “Software” specially designed or modified for the “use” of “UAVs” and associated systems, equipment and components specified in 9A012;

 

 f. “Software” specially designed to design the internal cooling passages of aero gas turbine blades, vans and tip shrouds;

 

 g. “Software” having all of the following:

 1. Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and

 2. Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions which have been validated with actual aero gas turbine engine (experimental or production) performance data.

 

 

9D101 “Software” specially designed or modified for the “use” of goods specified in 9B105, 9B106, 9B116 or 9B117.

 

 

9D103 “Software” specially designed for modelling, simulation or design integration of the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104, or the subsystems specified in 9A005, 9A007, 9A105.a., 9A106, 9A108, 9A116 or 9A119.

 Note: “Software” specified in 9D103 remains controlled when combined with specially designed hardware specified in 4A102.

 

 

9D104 “Software” specially designed or modified for the “use” of goods specified in 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A008.d., 9A009.a., 9A010.d., 9A011, 9A101, 9A102, 9A105, 9A106.c., 9A106.d., 9A107, 9A108.c., 9A109, 9A111, 9A115.a., 9A116.d., 9A117 or 9A118.

 

 

9D105 “Software” which coordinates the function of more than one subsystem, specially designed or modified for “use” in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

 

 

9E Technology

 

 Note: “Development” or “production” “technology” specified in 9E001 to 9E003 for gas turbine engines remains controlled when used as “use” “technology” for repair, rebuild and overhaul.  Excluded from control are: technical data, drawings or documentation for maintenance activities directly associated with calibration, removal or replacement of damaged or unserviceable line replaceable units, including replacement of whole engines or engine modules.

 

 

9E001 “Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 9A001.b., 9A004 to 9A012, 9A350, 9B or 9D.

 

 

9E002 “Technology” according to the General Technology Note for the “production” of

 equipment specified in  9A001.b., 9A004 to 9A011, 9A350 or 9B.

 

 N.B.: For “technology” for the repair of controlled structures, laminates or materials, see 1E002.f.

 

 

9E003 Other “technology” as follows:

 

 a. “Technology” “required” for the “development” or “production” of any of the following gas turbine engine components or systems:

 1. Gas turbine blades, vanes or tip shrouds made from directionally solidified (DS) or single crystal (SC) alloys and having (in the 001 Miller Index Direction) a stressrupture life exceeding 400 hours at 1,273 K (1,000°C) at a stress of 200 MPa, based on the average property values;

 2. Multiple domed combustors operating at average burner outlet temperatures exceeding 1,813 K (1,540°C) or combustors incorporating thermally decoupled combustion liners, nonmetallic liners or nonmetallic shells;

 3. Components manufactured from any of the following:

 a. Organic “composite” materials designed to operate above 588 K (315°C);

 b. Metal “matrix” “composite”, ceramic “matrix”, intermetallic or intermetallic reinforced materials specified in 1C007; or

 c. “Composite” material specified in 1C010 and manufactured with resins specified in 1C008;

 

 

9E003 a. continued

 

 4. Uncooled turbine blades, vanes, tipshrouds or other components, designed to operate at gas path total (stagnation) temperatures of 1,323 K (1,050°C) or more at sealevel static takeoff (ISA) in a ‘steady state mode’ of engine operation;

 5. Cooled turbine blades, vanes or tipshrouds, other than those described in 9E003.a.1., exposed to gas path total (stagnation) temperatures of 1,643 K (1,370°C) or more at sealevel static takeoff (ISA) in a ‘steady state mode’ of engine operation;

 

 Technical Note:

 The term ‘steady state mode’ defines engine operation conditions, where the engine parameters, such as thrust/power, rpm and others, have no appreciable fluctuations, when the ambient air temperature and pressure at the engine inlet are constant.

 

 6. Airfoiltodisk blade combinations using solid state joining;

 7. Gas turbine engine components using “diffusion bonding” “technology” specified in 2E003.b.;

 8. Damage tolerant gas turbine engine rotating components using powder metallurgy materials specified in 1C002.b.;

 9. “FADEC” for gas turbine and combined cycle engines and their related diagnostic components, sensors and specially designed components;

 10. Adjustable flow path geometry and associated control systems for:

 a. Gas generator turbines;

 b. Fan or power turbines;

 c. Propelling nozzles;

 Note 1: Adjustable flow path geometry and associated control systems in 9E003.a.10. do not include inlet guide vanes, variable pitch fans, variable stators or bleed valves for compressors.

 Note 2: 9E003.a.10. does not control “development” or “production” “technology” for adjustable flow path geometry for reverse thrust.

 11. Hollow fan blades.

 

 b. “Technology” “required” for the “development” or “production” of any of the following:

 1. Wind tunnel aeromodels equipped with nonintrusive sensors capable of transmitting data from the sensors to the data acquisition system; or

 2. “Composite” propeller blades or propfans capable of absorbing more than 2,000 kW at flight speeds exceeding Mach 0.55;

 

 c. “Technology” “required” for the “development” or “production” of gas turbine engine components using “laser”, water jet, ElectroChemical Machining (ECM) or Electrical Discharge Machines (EDM) hole drilling processes to produce holes having any of the following:

 1. All of the following:

 a. Depths more than four times their diameter;

9E003 c. continued

 

 b. Diameters less than 0.76 mm; and

 c. Incidence angles equal to or less than 25°; or

 2. All of the following:

 a. Depths more than five times their diameter;

 b. Diameters less than 0.4 mm; and

 c. Incidence angles of more than 25°;

 

 Technical Note:

 For the purposes of 9E003.c.,incidence angle is measured from a plane tangential to the airfoil surface at the point where the hole axis enters the airfoil surface.

 

 d. “Technology” “required” for the “development” or “production” of helicopter power transfer systems or tilt rotor or tilt wing “aircraft” power transfer systems;

 

 e. “Technology” for the “development” or “production” of reciprocating diesel engine ground vehicle propulsion systems having all of the following:

 1. ‘Box volume’ of 1.2 m3 or less;

 2. An overall power output of more than 750 kW based on 80/1269/EEC, ISO 2534 or national equivalents; and

 3. Power density of more than 700 kW/m3 of ‘box volume’;

 

 Technical Note:

 ‘Box volume’ in 9E003.e. is the product of three perpendicular dimensions measured in the following way:

Length: The length of the crankshaft from front flange to flywheel face;

Width: The widest of the following:

 a. The outside dimension from valve cover to valve cover;

 b. The dimensions of the outside edges of the cylinder heads; or

 c. The diameter of the flywheel housing;

Height: The largest of any of the following:

 a. The dimension of the crankshaft centreline to the top plane of the valve cover (or cylinder head) plus twice the stroke; or

 b. The diameter of the flywheel housing.

 

 f. “Technology” “required” for the “production” of specially designed components for high output diesel engines, as follows:

 1. “Technology” “required” for the “production” of engine systems having all of the following components employing ceramics materials specified in 1C007:

 a. Cylinder liners;

 b. Pistons;

 c. Cylinder heads; and

9E003 f. continued

 

 d. One or more other components (including exhaust ports, turbochargers, valve guides, valve assemblies or insulated fuel injectors);

 

 2. “Technology” “required” for the “production” of turbocharger systems with singlestage compressors and having all of the following:

 a. Operating at pressure ratios of 4:1 or higher;

 b. Mass flow in the range from 30 to 130 kg per minute; and

 c. Variable flow area capability within the compressor or turbine sections;

 

 3. “Technology” “required” for the “production” of fuel injection systems with a specially designed multifuel (e.g., diesel or jet fuel) capability covering a viscosity range from diesel fuel (2.5 cSt at 310.8 K (37.8°C)) down to gasoline fuel (0.5 cSt at 310.8 K (37.8°C)) and having all of the following:

 a. Injection amount in excess of 230 mm3 per injection per cylinder; and

 b. Electronic control features specially designed for switching governor characteristics automatically depending on fuel property to provide the same torque characteristics by using the appropriate sensors;

 

 g. “Technology” “required” for the “development” or “production” of high output diesel engines for solid, gas phase or liquid film (or combinations thereof) cylinder wall lubrication and permitting operation to temperatures exceeding 723 K (450°C), measured on the cylinder wall at the top limit of travel of the top ring of the piston.

 

 Technical Note:

 High output diesel engines’ are diesel engines with a specified brake mean effective pressure of 1.8 MPa or more at a speed of 2,300 r.p.m., provided the rated speed is 2,300 r.p.m. or more.

 

 

9E101 “Technology” according to the General Technology Note for the “development” or “production” of goods specified in 9A101, 9A102, 9A104 to 9A111 or 9A115 to 9A119.

 

 

9E102 “Technology” according to the General Technology Note for the “use” of space launch vehicles specified in 9A004, or goods specified in 9A005 to 9A011, 9A101, 9A102, 9A104 to 9A111, 9A115 to 9A119, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9D103.

 

SENSITIVE LIST OF DUALUSE GOODS AND TECHNOLOGIES

 

 

 

Note This List contains a subset of the Items controlled in Categories 1 to 9 of the Part 2 List of DualUse Goods and Technologies. The items in this List are considered to be sensitive, requiring additional care in their transfer. General Export Licences are generally not available for the export of the following sensitive goods.

 

N.B.: Where abbreviated entries are used, see Part 2 for full details. Text that differs from that in Part 2 is in bold type.

 

Category 1

 

 

 

1A002

“Composite” structures or laminates...

 

 

1A007

Equipment and devices, specially designed to initiate charges and devices containing energetic materials, by electrical means, as follows:

N.B.: SEE ALSO ML4.a., ML4.b., ML909, 3A229 AND 3A232.

a. Explosive detonator firing sets designed to drive multiple controlled explosive detonators specified in 1A007.b. below;

 

b. Electrically driven explosive detonators as follows:

  1.        Exploding bridge (EB);
  2.        Exploding bridge wire (EBW);
  3.        Slapper;
  4.        Exploding foil initiators (EFI).

Note:  1A007.b. does not control detonators using only primary explosives, such as lead azide.

 

 

1C001

Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers.

N.B.: SEE ALSO 1C101

 

 

1C007.c. & 1C007.d.

Ceramicceramic “composite” materials...

1C010.c. & 1C010.d.

Fibrous or filamentary materials...

1C012

Materials as follows...

 

 

Materials or devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures; not controlled in 1C001, usable in ‘missiles’, “missile” subsystems or “unmanned aerial vehicles” specified in 9A012.

 

Note: 1C101 does not control materials if such goods are formulated solely for civil applications.

 

Technical Note:

In 1C101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

 

1C239

High explosives, not controlled in the Munitions List, or substances or mixtures containing more than 2% thereof, with a crystal density greater than 1.8 gm/cm³ and having a detonation velocity greater than 8000 m/s.

 

 

“Software” for the “development” of organic “matrix”, metal “matrix” or carbon “matrix” laminates or “composites” listed in this List.

 

“Software” specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.

 

 

1E001

“Technology” according to the General Technology Note for the “development” or “production” of equipment and materials in 1A002 or 1C of this List.

 

 

1E002.e. & 1E002.f.

Other “technology”...

1E101

“Technology” according to the GTN for the “use” of goods specified in 1C101 or 1D103.

 

 

1E102

“Technology” according to the GTN for the “development” of “software” specified in 1D103.

 

 

1E201

“Technology” according to the General Technology Note for the “use” of goods specified in 1C239.

 

 

Category 2

 

 

 

2B001.a.

Deleted

2B001.b.

Deleted

2B001.d.

Deleted

2B001.f.

Deleted

 

 

2B003

Deleted

 

 

2D001

“Software”, other than that controlled by 2D002, specially designed for the “development” or “production” of the following equipment:

 

a. Machine tools for turning, having all of the following characteristics:

1. Positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; and

2. Two or more axes which can be coordinated simultaneously for “contouring control”.

 

b. Machine tools for milling, having any of the following characteristics:

1.a. Positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; and

b. Three linear axes plus one rotary axis which can be coordinated simultaneously for “contouring control”;

2. Five or more axes which can be coordinated simultaneously for “contouring control” and have a positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; or

3. A positioning accuracy for jig boring machines, with “all compensations available”, equal to or  less (better) than 3 µm according to ISO 230/2 (1997) or national equivalents along any linear axis;

 

c. Electrical discharge machines (EDM)....

 

d. Deepholedrilling machines....

 

e. “Numerically controlled” or manual machine tools...

 

 

2E001

“Technology” according to the General Technology Note for the “development” of equipment or “software” in 2D of this List or for the “development” of the following equipment:

 

a. Machine tools for turning, having all of the following characteristics:

1. Positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; and

2. Two or more axes which can be coordinated simultaneously for “contouring control”.

 

b. Machine tools for milling, having any of the following characteristics:

1.a. Positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; and

b. Three linear axes plus one rotary axis which can be coordinated simultaneously for “contouring control”;

2. Five or more axes which can be coordinated simultaneously for “contouring control” and have a positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; or

3. A positioning accuracy for jig boring machines, with “all compensations available”, equal to or  less (better) than 3 µm according to ISO 230/2 (1997) or national equivalents along any linear axis;

 

c. Electrical discharge machines (EDM)....

 

d. Deepholedrilling machines....

 

e. “Numerically controlled” or manual machine tools...

2E002

“Technology” according to the General Technology Note for the “production” of the following equipment:

 

a. Machine tools for turning, having all of the following characteristics:

1. Positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; and

2. Two or more axes which can be coordinated simultaneously for “contouring control”.

 

b. Machine tools for milling, having any of the following characteristics:

1.a. Positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; and

b. Three linear axes plus one rotary axis which can be coordinated simultaneously for “contouring control”;

2.             Five or more axes which can be coordinated simultaneously for “contouring control” and have a positioning accuracy with “all compensations available” equal to or less (better) than 3.6 µm according to ISO 230/2 (1997) or national equivalents along any linear axis; or

3. A positioning accuracy for jig boring machines, with “all compensations available”, equal to or  less (better) than 3 µm according to ISO 230/2 (1997) or national equivalents along any linear axis;

 

c. Electrical discharge machines (EDM)....

 

d. Deepholedrilling machines....

 

e. “Numerically controlled” or manual machine tools...

 

 

Category 3

 

 

 

3A002.g.2.

Atomic frequency standards....

 

 

3A229

Highcurrent pulse generators, as follows…

N.B.: SEE ALSO ML4.a.,b., ML909

3A232

Multipoint initiation systems, other than those specified in 1A007 above, as follows…

N.B.: SEE ALSO ML4.a.

 

 

3B001.a.2.

Metal organic chemical vapour deposition reactors....

 

 

3D001

“Software” specially designed for the “development” or “production” of equipment in 3A002.g. or 3B of this List.

3E001

“Technology” according to the General Technology Note for the “development” or “production” of equipment in 3A or 3B of this List.

 

 

3E201

“Technology” according to the General Technology Note for the “use” of equipment specified in 3A229 or 3A232.

 

 

Category 4

 

 

 

4A001.a.2.

Electronic computers......radiation hardened;

 

 

4A003.b.

Deleted

4A003.c.

Deleted

 

 

4D001

“Software” specially designed for the “development” or “production” of equipment in 4A of this List or for the “development” or “production” of “digital computers” having an “Adjusted Peak Performance” (“APP”) exceeding 0.1 Weighted TeraFLOPS (WT).

 

 

4E001

“Technology” according to the General Technology Note for the “development” or “production” of the following equipment or “software”:

 Equipment in 4A of this List;

 “Digital computers” having an “Adjusted Peak Performance” (“APP”) exceeding 0.1 Weighted TeraFLOPS (WT); or

 “Software” in 4D of this List.

 

 

Category 5 Part 1

 

 

 

5A001.b.3.

Being radio equipment .......

5A001.b.5.

Being digitally controlled radio receivers...

 

 

5B001.a.

Equipment and specially designed components or accessories therefor, specially designed for the “development”, “production” or “use” of equipment, functions or features in Category 5 Part 1 of this List.

 

 

5D001.a.

“Software” specially designed for the “development” or “production” of equipment, functions or features in Category 5 Part 1 of this List.

 

5D001.b.

 

“Software” specially designed or modified to support “technology” listed under 5E001 of this List.

 

 

5E001.a.

“Technology” according to the General Technology Note for the “development” or “production” of equipment, functions, features or “software” in Category 5 Part 1 of this List.

 

 

Category 5 Part 2

 

 

 

5A002.a.2.

Equipment designed or modified to perform cryptanalytic functions.

 

5D002.c.1.

 

Only software having the characteristics, or performing or simulating the functions, of equipment specified in 5A002.a.2.

 

 

5E002

Only “technology” for the “development”, “production” or “use” of the goods specified in 5A002.a.2. or 5D002.c.1. above.

Category 6

 

 

 

6A001.a.1.b.

Object detection or location systems having any of the following:

1. A transmitting frequency below 5 kHz or a sound pressure level exceeding 224 dB (reference 1 µPa at 1 m) for equipment with an operating frequency in the band from 5 kHz to 10 kHz inclusive;

2. Sound pressure level exceeding 224 dB (reference 1 Pa at 1 m) for equipment with an operating frequency in the band from 10 kHz to 24 kHz inclusive;

3. Sound pressure level…;

4. Forming beams of …;

5. Designed to operate…

6. Designed to withstand…;

 

 

6.A.1.a.2.a.1.

6.A.1.a.2.a.2.

6.A.1.a.2.a.3.

6.A.1.a.2.a.5.

6.A.1.a.2.a.6.

 

Hydrophones...Incorporating…

Hydrophones...Incorporating flexible assemblies…

Hydrophones...Having any...

Hydrophones...When designed...

Hydrophones...Designed for...

 

 

 

6A001.a.2.b.

Towed acoustic hydrophone arrays...

 

 

6A001.a.2.c.

Processing equipment, specially designed for real time application with towed acoustic hydrophone arrays, having “user accessible programmability” and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beamforming using Fast Fourier or other transforms or processes;

 

 

6A001.a.2.d.

Heading sensors....

 

 

6A001.a.2.e.

 

Bottom or bay cable systems having any of the following:

1. Incorporating hydrophones... or

2. Incorporating multiplexed hydrophone group signal modules…;

6A001.a.2.f.

Processing equipment, specially designed for real time application with bottom or bay cable systems, having “user accessible programmability” and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beamforming using Fast Fourier or other transforms or processes;

 

 

6A002.a.1.a.,b., and c.

“Spacequalified” solidstate detectors.....

 

 

6A002.a.2.a.

Image intensifier tubes ...

1. A peak response…

2. Electron image amplification…

3. Photocathodes, as follows:

a. S20, S25 or multialkali photocathodes with a luminous sensitivity exceeding 700 lm;

b. GaAs or GaInAs photocathodes;

c.       Other IIIV compound semiconductor photocathodes.

6.A.2.a.2.b.

Image intensifier tubes…

 

 

6A002.a.3.

Nonspace qualified “focal plane arrays”…;

 

Note 3

6A002.a.3. does not apply to the following “focal plane arrays” in this List:

 

a. Platinum Silicide (PtSi) “focal plane arrays” having less than 10,000 elements;

 

b. Iridium Silicide (IrSi) “focal plane arrays”.

 

 

 

Note 4

6A002.a.3. does not apply to the following “focal plane arrays” in this List:

 

a. Indium Antimonide (InSb) or Lead Selenide (PbSe) “focal plane arrays” having less than 256 elements;

 

b. Indium Arsenide (InAs) “focal plane arrays”;

 

c. Lead Sulphide (PbS) “focal plane arrays”;

 

d. Indium Gallium Arsenide (InGaAs) “focal plane arrays”.

 

 

 

Note 5

6A002.a.3. does not apply to Mercury Cadmium Telluride (HgCdTe) “focal plane arrays” as follows in this List:

 

a. ‘Scanning Arrays’ having any of the following:

 

 1. 30 elements or less; or 

 

 2. Incorporating time delayandintegration within the element and having 2 elements or less;

 

b. ‘Staring Arrays’ having less than 256 elements.

 

 

 

Technical Notes

  1. ‘Scanning Arrays’ are defined as “focal plane arrays” designed for use with a scanning optical system that images a scene in a sequential manner to produce an image;

 

2.     ‘Staring Arrays’ are defined as “focal plane arrays” designed for use with a nonscanning optical system that images a scene.

 

 

 

Note 6

6A002.a.3. does not apply to the following “focal plane arrays” in this List:

 

a. Gallium Arsenide (GaAs) or Gallium Aluminum Arsenide (GaAlAs) quantum well “focal plane arrays” having less than 256 elements;

 

b. Microbolometer “focal plane arrays” having less than 8,000 elements.

 

 

 

Note 7

6A002.a.3.g. does not apply to the linear (1dimensional) “focal plane arrays” specially designed or modified to achieve ‘charge multiplication’ having 4,096 elements or less.

 

 

 

Note 8

6A002.a.3.g. does not apply to the nonlinear (2dimensional) “focal plane arrays” specially designed or modified to achieve ‘charge multiplication’ having a maximum linear dimension of 4,096 elements and a total of 250,000 elements or less.

 

 

6A002.b.

“Monospectral imaging sensors” and “multispectral imaging sensors”....

 

 

6A002.c.

‘Direct view’ imaging equipment incorporating any of the following:

1. Image intensifier tubes having the characteristics listed in 6A002.a.2.a. or 6A002.a.2.b. of this List;

2. “Focal plane arrays” having the characteristics listed in 6A002.a.3. of this List or 6A002.e.; or

3. Solidstate detectors having the characteristics listed in 6A002.a.1.;

 

 

6A002.e.

Deleted

 

 

6A003.b.3

Imaging cameras incorporating image intensifier tubes having the characteristics listed in 6A002.a.2.a. or 6A002.a.2.b. of this List;

6A003.b.4

Imaging cameras incorporating “focal plane arrays” having any of the following:

 

a.  Incorporating “focal plane arrays” specified by 6A002.a.3.a. to 6A002.a.3.e. of this List;

 

b. Incorporating “focal plane arrays” specified by 6A002.a.3.f. of this List;

 

c. Incorporating “focal plane arrays” listed in 6A002.a.3.g. of this List; or

 

d. Incorporating “focal plane arrays” specified by 6A002.e.

 

Note 1 ‘Imaging cameras’ described in 6A003.b.4 include “focal plane arrays” combined with sufficient signal processing electronics, beyond the read out integrated circuit, to enable as a minimum the output of an analogue or digital signal once power is supplied.

 

Note 2 6A003.b.4.a. does not control imaging cameras incorporating linear “focal plane arrays” with twelve elements or fewer, not employing timedelayandintegration within the element, designed for any of the following:

 

a. Industrial or civilian intrusion alarm, traffic or industrial movement control or counting systems;

 

b. Industrial equipment used for inspection or monitoring of heat flows in buildings, equipment or industrial processes;

 

c. Industrial equipment used for inspection, sorting or analysis of the properties of materials;

 

d. Equipment specially designed for laboratory use; or

 

e.         Medical equipment.

 

Note 3 6A003.b.4.b. does not control imaging cameras having any of the following characteristics:

 

a.  A maximum  frame rate equal to or less than 9 Hz;

 

b.   Having all of the following:

 

1. Having a minimum horizontal or vertical InstantaneousFieldofView (IFOV) of at least 10 mrad/pixel (milliradians/pixel);

 

2. Incorporating a fixed focallength lens that is not designed to be removed;

 

3.  Not incorporating  a direct view display; and

 

Technical Note:

‘Direct view’ refers to an imaging camera operating in the infrared spectrum that presents a visual image to a human observer using a neartoeye micro display incorporating any lightsecurity mechanism.

 

4.  Having any of the following:

 

a.   No facility  to obtain a viewable image of the detected fieldofview; or

 

b.  The camera is designed for a single kind of application and designed not to be user modified; or

 

Technical Note

Instantaneous Field of View (IFOV) specified in Note 3.b. is the lesser figure of the Horizontal FOV or the Vertical FOV.

Horizontal IFOV = horizontal Field of View (FOV)/number of horizontal detector elements

Vertical IFOV= vertical Field of View (FOV)/number of vertical detector elements.

 

c. Where the camera is specially designed for installation into a civilian passenger land vehicle of less than three tonnes (gross vehicle weight) and having all of the following:

 

1. Is only operable when installed in any of the following:

 

a. The civilian passenger land vehicle for which it was intended; or

 

b.  A specially designed, authorized maintenance test facility; and

 

2.  Incorporates an active mechanism that forces the camera not to function when it is removed from the vehicle for which it was intended.

 

Note: When necessary, details of the item will be provided, upon request, to the appropriate authority in the exporter’s country in order to ascertain compliance with the conditions described in Note 3.b.4.  and Note 3.c. above.

 

 

 

Note 4 6A003.b.4.c. does not apply to ‘imaging cameras’ having any of the following characteristics:

 

a. Having all of the following:

 

1. Where the camera is specially designed for installation as an integrated component into indoor and wallplugoperated systems or equipment, limited by design for a single kind of application, as follows:

 

a. Industrial process monitoring, quality control, or analysis of the properties of materials;

 

b. Laboratory equipment specially designed for scientific research;

 

c. Medical equipment; or

 

d. Financial fraud detection equipment; and

 

2. Is only operable when installed in any of the following:

 

a. The system(s) or equipment for which it was intended; or

 

b. A specially designed, authorised maintenance facility; and

 

3. Incorporates an active mechanism that forces the camera not to function when it is removed from the system(s) or equipment for which it was intended;

 

b. Where the camera is specially designed for installation into a civilian passenger land vehicle of less than three tonnes (gross vehicle weight), or passenger and vehicle ferries having a length overall (LOA) 65 m or greater, and having all of the following:

 

1. Is only operable when installed in any of the following:

 

a. The civilian passenger land vehicle or passenger and vehicle ferry for which it was intended; or

 

b. A specially designed, authorised maintenance test facility; and

 

2. Incorporates an active mechanism that forces the camera not to function when it is removed from the vehicle for which it was intended;

 

c. Limited by design to have a maximum radiant sensitivity of 10 mA/W or less for wavelengths exceeding 760 nm, having all of the following:

 

1. Incorporating a response limiting mechanism designed not to be removed or modified; and

 

2. Incorporates an active mechanism that forces the camera not to function when the response limiting mechanism is removed; or

 

d. Having all of the following:

 

1. Not incorporating a ‘direct view’ or electronic image display;

 

2. Has no facility to output a viewable image of the detected field of view;

 

3. The “focal plane array” is only operable when installed in the camera for which it was intended; and

 

4. The “focal plane array” incorporates an active mechanism that forces it to be permanently inoperable when removed from the camera for which it was intended.

 

 

 

Note When necessary, details of the item will be provided, upon request, to the appropriate authority in the exporter’s country in order to ascertain compliance with the conditions described in Note 4 above.

 

 

6A003.b.5.

Imaging cameras incorporating solidstate detectors specified by 6A002.a.1.;

 

 

6A004.c.

“Spacequalified” components for optical systems....

6A004.d.

Optical control equipment.....

 

 

6A006.a.

Deleted

6A006.a.1.

“Magnetometers”... Using “superconductive” (SQUID) “technology”...

6A006.a.2.

“Magnetometers” … Using optically pumped or nuclear precession (proton/Overhauser) “technology” having a “noise level” (sensitivity) lower (better) than 2pT rms per square root Hz;

 

6A006.d.

 

“Compensation systems” for the following:

 

1. Magnetic sensors controlled in 6A006.a.2. using optically pumped or nuclear precession (proton/Overhauser) “technology” that will permit these sensors to realize a “noise level” (sensitivity) lower (better) than 2 pT rms per square root Hz.

 

2. Underwater electric field sensors controlled in 6A006.b.

 

3. Magnetic gradiometers controlled in 6A006.c. that will permit these sensors to realize a “noise level” (sensitivity) lower (better) than 3 pT/m rms per square root Hz.

 

6A006.g.

 

Deleted

 

6A006.h.

 

Deleted

 

6A008.d.

 

Radar systems....Capable of…

6A008.h.

Radar systems…Employing processing

6A008.k.

Radar systems…Having “signal processing”…

6A008.l.3.

Radar systems…Having data processing… Processing for…

 

 

6B008

Pulse radar crosssection measurement systems having transmit pulse widths of 100 ns or less and specially designed components therefor.

N.B.: SEE ALSO 6B108

 

6B108

Systems specially designed for radar cross section measurement usable for “missiles” and their subsystems.

 

 

6D001

“Software” specially designed for the “development” or “production” of equipment in 6A004, 6A008 or 6B008 of this List.

 

 

6D003.a.

“Software”, as follows…

 

 

6E001

“Technology” according to…

 

 

6E002

“Technology” according to the General Technology Note for the “production” of equipment in 6A or 6B of this List.

 

Category 7

 

 

 

“Guidance sets”, usable in “missiles” capable of achieving system accuracy of 3.33% or less of the range (e.g., a “CEP” of 10 km or less at a range of 300 km), except “guidance sets” designed for missiles with a range under 300 km or manned aircraft.

 

 

Test, calibration or alignment equipment specially designed for equipment specified in 7A117 above.

Note:  7B001 does not control test, calibration or alignment equipment for Maintenance Level I or Maintenance Level II.

 

Equipment specially designed for the “production” of equipment specified in 7A117 above.

 

“Production facilities” specially designed for equipment specified in 7A117 above.

 

7D002

“Source code” for the “use”…

 

 

7D003.a.

“Software” specially designed or modified to…

7D003.b.

“Source code” for…

7D003.c.

“Source code” for…

7D003.d.1. to 4. & 7.

“Source code” for the “development” of…

 

 

7D101

“Software” specially designed for the “use” of equipment specified in 7B003 or 7B103 above.

 

 

7E001

“Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 7A117, 7B003, 7B103 or 7D101 above.

 

 

7E002

“Technology” according to the General Technology Note for the “production” of equipment specified in 7A117, 7B003 and 7B103 above.

 

 

7E101

“Technology” according to the General Technology Note for the “use” of equipment specified in 7A117, 7B003, 7B103 and 7D101 above.

 

 

Category 8

 

 

 

8A001.b.

Manned, untethered submersible vehicles…

8A001.c.

Unmanned, tethered submersible vehicles.....

8A001.d.

Unmanned, untethered submersible vehicles...

 

 

8A002.b.

Systems specially designed or modified for the automated control of the motion of submersible vehicles in 8A001 of this List using navigation data and having closed loop servocontrols:

1. Enabling…;

2. Maintaining…; or

3. Maintaining…;

 

8A002.h.

 

“Robots” specially designed for underwater use......

8A002.j.

Air independent power systems.......

8A002.o.3.

Noise reduction systems designed for use on vessels of 1000 tonnes displacement...

8A002.p.

Pumpjet propulsion systems....

 

 

8D001

“Software” specially designed for the “development” or “production” of equipment in 8A of this List.

 

 

8D002

Specific “software”........

 

 

8E001

“Technology” according to the General Technology Note for the “development” or “production” of equipment in 8A of this List.

 

 

8E002.a.

“Technology” for the “development”, “production”, repair, overhaul or refurbishing (remachining) of propellers specially designed for underwater noise reduction.

 

 

Category 9

 

 

 

9A004

Space launch vehicles capable of delivering at least a 500 kg payload to a range of at least 300 km.

N.B.: SEE ALSO 9A104.

Note 1: 9A004 does not control payloads.

 

 

9A005

Liquid rocket propulsion systems containing any of the systems or components specified in 9A006 usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below.

N.B.: SEE ALSO 9A105 and 9A119.

 

 

9A007.a.

Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below, with any of the following:

N.B.: SEE ALSO 9A119.

 

a. Total impulse capacity exceeding 1.1 MNs;

 

 

9A008.d.

Components, as follows, specially designed for solid rocket propulsion systems:

N.B.: SEE ALSO 9A108.c.

 

d. Movable nozzle or secondary fluid injection thrust vector control systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below, capable of any of the following:

1. Omniaxial movement exceeding ± 5°;

2. Angular vector rotations of 20°/s or more; or

3. Angular vector accelerations of 40°/s2 or more.

 

 

9A011

Ramjet, scramjet or combined cycle engines...

 

 

9A104

Sounding rockets, capable of delivering at least a 500 kg payload to a range of at least 300 km.

N.B.: SEE ALSO 9A004.

9A105.a.

Liquid propellant rocket engines, as follows:

N.B.: SEE ALSO 9A119.

 

a. Liquid propellant rocket engines usable in “missiles”, other than those specified in 9A005, having a total impulse capacity equal to or greater than 1.1 MNs; except liquid propellant apogee engines designed or modified for satellite applications and having all of the following:

1. nozzle throat diameter of 20 mm or less; and

2. combustion chamber pressure of 15 bar or less.

 

 

9A106.c.

Systems or components, other than those specified in 9A006, usable in “missiles”, as follows, specially designed for liquid rocket propulsion systems:

c. Thrust vector control subsystems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km.

Technical Note:

Examples of methods of achieving thrust vector control specified in 9A106.c. are:

1. Flexible nozzle;

2. Fluid or secondary gas injection;

3. Movable engine or nozzle;

4. Deflection of exhaust gas stream (jet vanes or probes); or

5. Thrust tabs.

 

 

9A108.c.

Components, not controlled in 9A008, usable in “missiles” as follows, specially designed for solid rocket propulsion systems:

 

c. Thrust vector control subsystems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km.

 

Technical Note:

Examples of methods of achieving thrust vector control specified in 9A108.c. are:

1. Flexible nozzle;

2. Fluid or secondary gas injection;

3. Movable engine or nozzle;

4. Deflection of exhaust gas stream (jet vanes or probes); or

5. Thrust tabs.

9A116

Reentry vehicles, usable in “missiles”, and equipment designed or modified therefor, as follows, except for reentry vehicles designed for nonweapon payloads:

 

a. Reentry vehicles;

b. Heat shields and components therefor fabricated of ceramic or ablative materials;

c. Heat sinks and components therefor fabricated of lightweight, high heat capacity materials;

d. Electronic equipment specially designed for reentry vehicles.

 

 

9A119

Individual rocket stages, usable in complete rocket systems or “unmanned aerial vehicles”, capable of delivering at least a 500 kg payload to a range of 300 km, other than those specified in 9A005 or 9A007.a. above.

 

 

9B001.b.

Ceramic cores or shells

 

 

9B115

Specially designed “production equipment” for the systems, subsystems and components specified in 9A005, 9A007.a., 9A008.d., 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above.

 

 

9B116

Specially designed “production facilities” for the space launch vehicles specified in 9A004, or systems, subsystems, and components specified in 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above.

 

 

9D001

“Software” specially designed or modified for the “development” of equipment or “technology” in 9A, 9B or 9E003 of this List.

 

 

9D002

“Software” specially designed or modified for the “production” of equipment in 9A or 9B of this List.

 

 

9D004.a.

Other “software”…2D or 3D…

9D004.c.

Other “software”…”Software” specially…

 

 

9D101

“Software” specially designed for the “use” of goods specified in 9B116 above.

 

 

9E001

“Technology” according to the General Technology Note for the “development” of equipment or “software” specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115, 9B116 or 9D101 above.

 

 

9E002

“Technology” according to the General Technology Note for the “production” of equipment specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115 or 9B116 above.

Note: For “technology” for the repair of controlled structures, laminates or materi als, see 1E002.f.

 

 

9E003.a.1.

Other “technology”…Gas turbine blades…

9E003.a.2. to 5. & 9E003.a.8., 9.E.3.a.9.

Other “technology”…

 

 

9E101

“Technology” according to the General Technology Note for the “development” or “production” of goods specified in 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above.

 

 

9E102

“Technology” according to the General Technology Note for the “use” of space launch vehicles specified in 9A004, 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116, 9A119, 9B115, 9B116 or 9D101 above.

 

 

VERY SENSITIVE LIST OF DUALUSE GOODS AND TECHNOLOGIES

 

 

 

Note This List is a subset of the items contained in the Sensitive List. The items in this List are considered to be very sensitive, requiring extreme care in their transfer. General Export Licences are not available for the export of the following very sensitive goods.

 

N.B. Where abbreviated entries are used, see Part 2 for full details. Text that differs from that in Part 2 is in bold type.

 

Category 0

All of Category 0 of Part 2 is included in the Very Sensitive List.

 

N.B.: For 0C003 and 0C004, only if for use in a “nuclear reactor” (within 0A001.a.).

Category 1

 

1A002.a.

“Composite” structures or laminates consisting of an organic “matrix” and materials specified by 1.C.10.c. or 1.C.10.d .

 

 

1B226

Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.

 

Note:  1B226 includes separators:

 

 a. Capable of enriching stable isotopes;

 

 b.  With the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.

1B231

Tritium facilities or plants, and equipment therefor, as follows:

a. Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;

b. Equipment for tritium facilities or plants, as follows:

 1.  Hydrogen or helium refrigeration units capable of    cooling to 23 K (250°C) or less, with heat removal                                           capacity greater than 150 W;

 2.  Hydrogen isotope storage or purification systems    using metal hydrides as the storage or purification                                           medium.

1B233

Lithium isotope separation facilities or plants, and equipment therefor, as follows:

a. Facilities or plants for the separation of lithium isotopes;

b.  Equipment for the separation of lithium isotopes, as  follows:

 1.  Packed liquidliquid exchange columns specially    designed for lithium amalgams;

 2.  Mercury or lithium amalgam pumps;

 3.  Lithium amalgam electrolysis cells;

 4.  Evaporators for concentrated lithium hydroxide   solution.

 

 

1C001

Materials specially designed for use as absorbers of electromagnetic waves...

 

 

1C012

Materials as follows...

 

 

1C233

Lithium enriched in the lithium6 (6Li) isotope to greater than its natural isotopic abundance, and products or devices containing enriched lithium, as follows:  elemental lithium, alloys, compounds, mixtures containing lithium, manufactures thereof, waste or scrap of any of the foregoing.

Note: 1C233 does not control thermoluminescent dosimeters.

Technical Note:

The natural isotopic abundance of lithium6 is approximately 6.5 weight % (7.5 atom %).

 

 

1C235

Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.

Note:  1C235 does not control a product or device containing less than 1.48 x 103 GBq (40 Ci) of tritium.

 

 

1C351.d.4.

Ricin

1C351.d.5.

Saxitoxin

 

 

1E001

“Technology” according to the General Technology Note for the “development” or “production” of equipment and materials in 1A002 or 1C012.b. of this List.

 

 

1E201

“Technology” according to the General Technology Note for the “use” of goods specified in  1B226, 1B231, 1B233, 1C233 or 1C235.

 

 

 

Category 2

None

Category 3

 

 

 

3A228

Switching devices, as follows:

a. Coldcathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:

 1. Containing three or more electrodes;

 2. Anode peak voltage rating of 2.5 kV or more;

 3. Anode peak current rating of 100 A or more; and

 4. Anode delay time of 10 µs or less;

 Note: 3A228 includes gas krytron tubes and vacuum sprytron tubes.

b. Triggered sparkgaps having both of the following characteristics:

  1.            An anode delay time of 15 µs or less; and
  2.            Rated for a peak current of 500 A or more;

 

 

3A231

Neutron generator systems, including tubes, having both of the following characteristics:

a. Designed for operation without an external vacuum system; and

b. Utilizing electrostatic acceleration to induce a tritiumdeuterium nuclear reaction

 

 

3E201

“Technology” according to the General Technology Note for the “use” of equipment specified in 3A228.a., 3A228.b. or 3A231.

 

 

Category 4

None

 

 

Category 5 Part 1

 

 

 

5A001.b.5.

Digitally controlled radio receivers...

 

 

5D001.a.

“Software” specially designed for the “development” or “production” of equipment, functions or features in Category 5 – Part 1 of this List.

 

 

5E001.a.

“Technology” according to the General Technology Note for the “development” or “production” of equipment, functions, features or “software” in Category 5 – Part 1 of this List.

 

 

Category 5 Part 2

None

 

 

Category 6

 

 

 

6A001.a.1.b.1.

Object detection or location systems having a sound pressure level exceeding 210 dB (reference 1 Pa at 1 m) and an operating frequency in the band from 30 Hz to 2 kHz.

 

 

6A001.a.2.a.1.

6A001.a.2.a.2.

6A001.a.2.a.3.

6A001.a.2.a.5.

6A001.a.2.a.6.

Hydrophones...Incorporating…

Hydrophones...Incorporating flexible assemblies…

Hydrophones...Having any…

Hydrophones...When designed...

Hydrophones...Designed for…

 

 

6A001.a.2.b.

Towed acoustic hydrophone arrays...

 

 

6A001.a.2.c.

Processing equipment, specially designed for real time application with towed acoustic hydrophone arrays, having “user accessible programmability”  and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beamforming using Fast Fourier or other transforms or processes;

 

 

6A001.a.2.e.

Bottom or bay cable systems having any of the following:

1. Incorporating hydrophones... or

2. Incorporating multiplexed hydrophone group signal modules …;

 

 

6A001.a.2.f.

Processing equipment, specially designed for real time application with bottom or bay cable systems, having “user accessible programmability”  and time or frequency domain processing and correlation, including spectral analysis, digital filtering and beamforming using Fast Fourier or other transforms or processes;

 

 

6A002.a.1.c.

“Spacequalified” solidstate detectors...

 

 

6A008.l.3.

Radar systems…Having data processing… Processing for…

 

 

6A203

Cameras and components, not controlled in 6A003, as follows:

a. Mechanical rotating mirror cameras, as follows, and specially  designed components therefor:

 1. Framing cameras with recording rates greater than    225,000 frames per second;

 2. Streak cameras with writing speeds greater than    0.5 mm per microsecond;

 Note: In 6A203.a. components of such cameras include their   synchronizing electronics units and rotor assemblies

 consisting of turbines, mirrors and bearings.

 

 

6A225

Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.

Note: 6A225 includes velocity interferometers such as VISARs

 (Velocity interferometer systems for any reflector) and DLIs

 (Doppler laser interferometers).

 

 

6A226

Pressure sensors, as follows:

a. Manganin gauges for pressures greater than 10 GPa;

b. Quartz pressure transducers for pressures greater than 10 GPa.

 

 

6B008

Pulse radar crosssection…

 

 

6D001

“Software” specially designed for the “development” or “production” of equipment in 6A008, or 6B008 of this List.

 

 

6D003.a.

“Software”, as follows:…

 

 

6E001

“Technology” according to the General Technology Note for the “development” of equipment or “software” in 6A, 6B, or 6D of this List.

 

 

6E002

“Technology” according to the General Technology Note for the “production”  of equipment in 6A or 6B of this List.

 

 

Category 7

 

 

 

7D003.a.

“Software”  specially designed or modified to…

7D003.b.

“Source code” for…

 

 

Category 8

 

 

 

8A001.b.

Manned, untethered submersible vehicles...

8A001.d.

Unmanned, untethered submersible vehicles...

 

 

8A002.o.3.b.

Active noise reduction or cancellation systems...

 

 

8D001

“Software” specially designed for the “development” or “production” of equipment in 8A of this List.

 

 

8E001

“Technology “according to the General Technology Note for the “development”  or “production”  of equipment in 8A of this List.

 

Category 9

 

 

 

9A011

Ramjet, scramjet or combined cycle engines...

 

 

9D001

“Software” specially designed or modified for the “development” of equipment or “technology” in 9A or 9E003 of this List.

 

 

9D002

“Software” specially designed or modified for the “production” of equipment in 9A of this List.

 

 

9E001

“Technology” according to the General Technology Note for the “development” of equipment or “software” in 9A011 or 9D of this List.

 

 

9E002

“Technology” according to the General Technology Note for the “production” of equipment in 9A011 of this List.

 

 

9E003.a.1.

Other “technology”…Gas turbine blades…

9E003.a.3.a.

“Technology” “required” for …

Components manufactured from...

Organic “composite” materials designed to operate above 588 K (315°C).

 

INDEX OF DSGL 2010

 

 

>>1<<

1-(2-nitrotriazolo)-2-dinitromethylene hydrazine

     see NTNMH

1,1,3,3,3-pentafluoro-2-(trifluoromethyl)-1-propene....................1C450.a.2

1,1,3-trinitroazetidine

     see TNAZ

1,1-diamino-2,2-dinitroethylene

     see DADE

1,2,3-tris[1,2-bis(difluoroamino)ethoxy] propane

     see TVOPA

1,2,4-butanetriol

     see 1,2,4-trihydroxybutane

1,2,4-trihydroxybutane (CAS 3068-00-6)...............................ML8.g.8

1,2-bis (2-chloroethylthio) ethane (CAS 3563-36-8)......................ML7.b.2

1,3,3-trinitroazetidine

     see TNAZ

1,3,5,7-tetraacetyl-1,3,5,7,-tetraaza cyclo-octane

     see TAT

1,3,5,7-tetranitro-1,3,5,7-tetraza-cyclooctane

     see HMX and derivatives

1,3,5-trichlorobenzene (CAS 108-70-3)................................ML8.g.7

1,3,5-trinitro-1,3,5-triaza-cyclohexane

     see RDX and derivatives

1,3-bis (2-chloroethylthio)-n-propane (CAS 63905-10-2)...................ML7.b.2

1,3-dinitro-1,3-diazetidine

     see DNAD

1,4,5,8-tetraazadecalin (CAS 5409-42-7)...............................ML8.g.6

1,4,5,8-tetranitro-1,4,5,8-tetraazadecalin

     see TNAD

1,4,5,8-tetranitro-pyridazino[4,5-d]pyridazine

     see TNP

1,4-bis (2-chloroethylthio)-n-butane (CAS 142868-93-7)...................ML7.b.2

1,4-dihydrazine nitrate

     see 3,6-dihydrazino tetrazine nitrate

1,4-dinitrodifurazanopiperazine

     see DDFP

1,5-bis (2-chloroethylthio)-n-pentane (CAS 142868-94-8)..................ML7.b.2

10-chloro-5,10-dihydrophenarsazine (CAS 578-94-9)............1A004.a.4, ML7.d.5

1-amino-3,5-dinitro-1,2,4-triazole

     see ADNT

1-fluoro-2,4-dinitroimidazole

     see FDIA

1-methyl-2-pyrrolidinone.............................................ML8

1-N-(2-nitrotriazolo) 3,5-dinitrotriazole

     see NTDNT

1-N-(2-nitrotriazolo)-4-nitrotetrazole

     see NTNT

1-picryl-2,4,5-trinitroimidazole

     see PTIA

1-picryl-3,5-dinitrotriazole

     see PDNT

>>===============================<<

>>2<<

2-(5-cyanotetrazolato) penta amine-cobalt (III) perchlorate

     see CP

2,2-dinitropropanol.................................................ML8

2,4,5-trichlorophenoxyacetic acid

     see Agent Orange

2,4,6,8-tetranitro-2,4,6,8-tetraazabicyclo [3,3,0]-octanone-3

     see K-55

2,4,6-trinitro-2,4,6-triazacyclohexanone

     see RDX and derivatives

2,4,6-trinitroresorcinol...............................................ML8

2,4,6-trinitrotoluene.................................................ML8

2,4-dichlorophenoxyacetic acid

     see Agent Orange

2,4-dinitroimidazole

     see DNI

2,6-bis(picrylamino)-3,5-dinitropyridine

     see PYX

2,6-diamino-3,5-dinitropyrazine-1-oxide

     see DDPO

2-chloro-1-phenylethanone (CAS 532-27-4)....................1A004.a.4, ML7.d.3

2-chloroethanol (CAS 107-07-3)......................................1C350

2-chloroethylchloromethylsulphide (CAS 2625-76-5).....................ML7.b.2

2-chlorophenyl methylene propanedinitrile...................1A004.a.4, ML7.d.2

2-chlorovinyldichloroarsine (CAS 541-25-3)............................ML7.b.2

2-hydroxyethylhydrazine nitrate...................................1C111.a.4

2-NDPA

     see 2-nitrodiphenylamine

2-nitrodiphenylamine.......................................1C111.c.3, ML8

2-nitroimino-5-nitro-hexahydro-1,3,5-triazine

     see NNHT

2-nitrotriazole 5-dinitramide

     see NTDNA

2-oxy-4,6-dinitroamino-s-triazine

     see DNAM

2-propenolato-1 methyl, n-propanolatomethyl butanolato-1, tris[dioctyl] pyrophosphate

     see titanium, titanium alloys and titanium compounds

>>===============================<<

>>3<<

3,3,7,7-tetrabis(difluoroamine) octahydro-1,5-dinitro-1,5-diazocine

     see TEDDZ

3,3-diamino-2,2,4,4,6,6-hexanitrobiphenyl

     see DIPAM

3,3-dinitro-5,5-bi-1,2,4-triazole

     see DBT

3,6-dihydrazino tetrazine nitrate...................................1C111.a.4

3-difluoroaminomethyl-3-azidomethyl oxetane

     see FAMAO

3-hydroxy-1-methylpiperidine (CAS 3554-74-3)..........................1C350

3-nitraza-1,5-pentane diisocyanate (CAS 7406-61-9).....................ML8.f.14

3-nitro-1,2,4-triazol-5-one

     see NTO

3-quinuclidinol (CAS 1619-34-7)......................................1C350

3-quinuclidinyl benzilate (CAS 6581-06-2).............................ML7.b.3

3-quinuclidone (CAS 3731-38-2)......................................1C350

>>===============================<<

>>4<<

4-amino-3,5-dihydrazino-1,2,4-triazole dinitramide

     see ADHTDN

4-hydroxybenzoic acid..........................................1C008.b.2

4-NDPA

     see 4-nitrodiphenylamine

4-nitrodiphenylamine...............................................ML8

>>===============================<<

>>5<<

5,7-diamino-4,6-dinitrobenzofurazane-1-oxide

     see CL-14

5-azido-2-nitrotriazole...........................................ML8.a.32

>>===============================<<

>>6<<

6-hydroxy-2 naphthoic acid, in thermoplastic liquid crystal copolymers....1C008.b.2

>>===============================<<

>>7<<

7-amino-4,6-dinitrobenzofurazane-1-oxide

     see ADNBF

>>===============================<<

>>A<<

ablative liners....................................................9A106

abradable materials, coating technology...............................2E003

abrin.......................................................1C351.d.12

absolute reflectance measurement equipment

     see reflectance measuring equipment

absorbers of electromagnetic waves

     see electromagnetic equipment

absorption and distillation columns

     see distillation and absorption columns

accelerometers.................................7A001, 7A101, 7A103, 7B003

accessories, for non-military firearms.................................ML904

acetyl ferrocenes..............................................1C111.c.6

acoustic systems, equipment and components

     see also underwater operations equipment

...............................................................6A001

     acoustic beacons.............................................6A001.a.1

     acoustic projectors............................................6A001.a.1

     acoustic vibration test equipment....................................9B006

     acoustic wave equipment..........................................3A001

     acoustic-optic signal processing equipment..........................3A001.c.3

     bulk acoustic wave equipment....................................3A001.c.2

     environmental chambers..........................................9B106

     hydrophones...............................6A001.a.2, 6A001.a.2, 6D003.a.2

     marine acoustic systems..........................................6A001

     noise reduction systems.....................................8A002, 8E002

     sonar navigation systems.................................6A001.a.2, 7A008

     surface acoustic wave equipment.................................3A001.c.1

actinides, crucibles resistant to......................................2A225

active flight control system systems and software

     see flight control systems

active magnetic bearing systems

     see bearings

active pulsed Doppler missile warning sensors...........................ML4

actively cooled mirrors

     see optical mirrors

adamsite

     see 10-chloro-5,10-dihydrophenarsazine

adaptive optics...................................................ML19

ADCS

     see analogue-to-digital converters

additives to fuels, explosives and propellants.............................ML8

adducted polymer ferrocene derivatives...............................ML8.f.4

ADHTDN (CAS 1614-08-0)........................................ML8.a.32

adjustable flow path geometry systems............................9E003.a.10

ADN (CAS 140456-78-6)...........................................ML8.d.1

ADNBF (CAS 97096-78-1)..........................................ML8.a.1

ADNT........................................................ML8.a.32

aerodynamic isotope separation systems

     see isotope separation plants, systems, equipment and components

aero-engines and components

     see also gas turbine engines

     fan turbine control systems.....................................9E003.a.10

     for military use..................................................ML10

     for missiles....................................................9A105

     for unmanned airborne vehicles..................................9A012.b.12

     gas turbine engines..............................................9A001

     jet combustion regulation equipment..................................9A118

     pulse jet engines................................................9A111

     superplastic forming and diffusion bonding tools.........................1B003

     turbofan engines..........................................9A101, 9A102

     turbojet engines.................................................9A101

     turboprop engines...............................................9A102

aerosol challenge testing chambers...................................2B352

aerosol generating units...........................................9A350

aflatoxins...................................................1C351.d.11

African horse sickness virus....................................1C352.a.17

African swine fever virus........................................1C352.a.1

Agent Orange...................................................ML7.b.4

agitators for use in reaction vessels..................................2B350

AHRS

     see attitude control equipment

air conditioning units, designed to filter toxic agents.....................ML7.f.1

air data systems......................................7D003.d.6, 7E004.a.2

air guns

     see also firearms and firearm components

..............................................................ML905

air independent power systems...............................8A002, ML9.b.4

air traffic control software.......................................6D003.d.1

airborne altimeters................................................7A006

airborne vehicles, equipment and components

     see aircraft and aircraft components

aircraft and aircraft components

     see also aero-engines and components

     see also navigation systems, equipment and components

     see also unmanned airborne vehicles, systems and components

...............................................................1B232

     equipment for the production of.....................................1B001

     for military use..................................................ML10

     global navigation satellite systems...................................7A105

     made from fluorinated compounds...................................1A001

     missile protection systems...........................................ML4

     navigation software..............................................7D003

     superplastic forming and diffusion bonding tools.........................1B003

aircraft engines

     see aero-engines and components

aircraft fuels

     see fuels and propellants and related equipment

aircraft simulators

     see simulators and simulator components

airfoil-to-disk combination joining equipment...................9B004, 9E003.a.6

Al--

     see aluminium, aluminium compounds and aluminium alloys

alane (CAS 7784-21-6)............................................ML8.c.2

alexandrite lasers...........................................6A005, 6C005

alkyl phosphonyl difluorides.......................................ML7.c.1

alkylated salts, as toxic agents..............................ML7.b.1, ML7.c.2

alkylphenylene ethers and thio-ethers..............................1C006.b.1

all wheel drive utility vehicles

     see also land vehicles and components

................................................................ML6

alloys

     see also name of metal, e.g. aluminium

...............................................................1C002

     equipment for the production of.....................................1B002

allylhydrazine, as propellant......................................1C111.a.4

alpha-bromobenzeneacetonitrile (CAS 5798-79-8)..............1A004.a.4, ML7.d.1

alpha-emitting radionuclides........................................1C236

altimeters.................................................7A006, 7A106

aluminium, aluminium compounds and aluminium alloys

     alloys...............................1C002.b.4, 1C002.c.1, 1C202, 2E003.b.2

     Al-Si-polyester coating technology...................................2E003

     alumina fibres..........................................1B001.d.4, 1C010

     aluminides...............................................1C002, 2E003

     aluminium hydride..............................................ML8.c.2

     aluminium oxides................................................1E.c.1

     conversion equipment.........................................1B001.d.4

     fibres made from Al2O3.........................................1C007.f.1

     spherical powdered fuel.................................1C111.a.1, ML8.c.8

     substrate materials...................................3C003, 3C005, 3C006

     superplastic forming and diffusion bonding tools for.......................1B003

     valves containing................................................2A226

amalgam electrolysis cells

     see electrolytic cells

aminodinitrobenzofuroxan

     see ADNBF

amiton (CAS 78-53-5)...........................................1C450.a.1

AMMO (CAS 90683-29-7)..........................................ML8.e.1

ammonia

     see nitrogen and nitrogen compounds

ammonia--hydrogen exchange plants (crackers)

     see also distillation and absorption columns

...........................................0B004.a.2, 0B004.b.3, 0B004.b.5

ammunition and components

     see also explosives and explosive devices

     see also firearms and firearm components

     for non-military firearms...........................................ML902

     for smooth-bore weapons...........................................ML3

     land vehicles for transportation of......................................ML6

amorphous alloy strips............................................1C003

amphibious vehicles................................................ML6

amplifiers, microwave

     see microwave equipment and components

amplifiers, solid state amplifiers...................................3A001.b.4

analogue computers, ruggedised.....................................4A101

analogue instrumentation tape recorders

     see recording equipment

analogue-to-digital converters................3A001.a.2, 3A001.a.5, 3A003, 4A003

analysers

     see network analysers

     see signal processing equipment

anechoic chambers...............................................9B106

angular accelerometers............................................7A001

angular measuring instruments

     see dimensional inspection and measuring systems

angular rate sensors..............................................7A002

angular--linear inspection equipment (hemishells)

     see dimensional inspection and measuring systems

animal pathogens.................................................1C352

anisotropic plasma dry etching equipment.............................3B001

anti-friction bearings and bearing systems.............................2A001

antimony compounds, subtrate materials containing................3C003, 3C004

anti-tank weapons..................................................ML2

AP (CAS 7790-98-9)..............................................ML8.d.2

approach parachutes............................................ML10.h.6

aramid fibres and filamentary materials................................1C210

arc remelt furnaces...............................................2B227

argon arc light systems, for underwater use.........................8A002.g.2

argon ion lasers..................................................6A205

armour

     see protective and decontamination clothing and equipment

armoured plate...................................................ML13

armoured vehicles and related equipment

     see also land vehicles and components

................................................................ML6

arms

     see firearms and firearm components

aromatic polyamide fibre technology.....................................1E

aromatic polyamide-imides..............................1C008.a.2, 1C008.a.3

aromatic polyetherimides........................................1C008.a.4

array processors

     see also signal processing equipment

...............................................................4A003

arsenic compounds

     arsenic trichloride  (CAS 7784-34-1)..................................1C350

     subtrate materials for integrated circuits..........................3C003, 3C004

aspheric optical elements..........................................6A004

asymmetric algorithm encryption equipment.........................5A002.a.1

ATC software

     see air traffic control software

atomic frequency standards.........................................3A002

atomic vapour laser isotope separation equipment

     see isotope separation plants, systems, equipment and components

attitude control equipment

     see also navigation systems, equipment and components

...............................................................7A116

Aujeszkys disease virus

     see porcine herpes virus

authentification equipment

     see also cryptographic equipment

...............................................................ML11

automatic loading multi-chamber central wafer handling systems...........3B001

automatic pilots..................................................7A103

automatic target tracking equipment..................................6A008

automatic weapons.................................................ML1

autonomous programmable airborne vehicles

     see unmanned airborne vehicles, systems and components

autonomous submersible vehicles

     see unmanned submersible vehicles

avian influenza virus............................................1C352.a.2

avionics EMP/EMI protection technology

     see electromagnetic equipment

avionics systems

     see aircraft and aircraft components

     see navigation systems, equipment and components

AVLIS

     see isotope separation plants, systems, equipment and components

azides and azide complexes..........................................ML8

azido groups, compounds containing................................ML8.e.6

azidomethylmethyloxetane and its polymers

     see AMMO

>>===============================<<

>>B<<

Bacillus anthracis..............................................1C351.c.1

bacterial cultures...........................................1C351, 1C354

baffles, for rotor tubes..........................................0B001.b.5

balancing machines...............................................2B119

ball and solid roller bearings

     see also bearings

...............................................................2A001

ballistic protection materials and components.......................ML13, ML6

BAMO (CAS 17607-20-4)..........................................ML8.e.2

band-pass filters

     see tunable band-pass filters

Bartonella quintana............................................1C351.b.2

base-ventilated propeller systems.................................8A002.o.2

basic copper salicylate (CAS 62320-94-9)..............................ML8.f.1

batch mixers with vacuum capabilities................................1B117

bathymetric survey systems......................................6A001.a.1

batteries (electrical)

     see cells and batteries (electrical)

bay cable systems.....................................6A001.a.2, 6D003.a.4

BCMO (CAS 142173-26-0)..........................................ML8.g.1

BDNPA (CAS 5108-69-0)...........................................ML8.e.3

BDNPF (CAS 5917-61-3)...........................................ML8.e.4

BDNTA.......................................................ML8.a.32

beam steering mirrors..........................................6A004.a.4

bearings

     active magnetic bearing systems....................................2A001

     anti-friction bearings and bearing systems..............................2A001

     ball bearings...................................................2A001

     magnetic bearings......................................2A001, 8A002.o.3

     magnetic suspension bearings...................................0B001.b.7

     pivot-cup assembly bearings.....................................0B001.b.8

     silent bearings...................................................ML9

     solid roller bearings..............................................2A001

bellows seal valves...............................................2A226

     for aerodynamic separation equipment.............................0B001.d.6

     for gas centrifuges...........................................0B001.b.13

     for gaseous diffusion separators..................................0B001.c.6

bellows, for rotor tube support....................................0B001.b.4

bellows-forming mandrels and dies

     see rotor assemblies for gas centrifuges

benzilic acid (CAS 76-93-7)..........................................1C350

benzyl bromide....................................................ML7

benzyl iodide......................................................ML7

beryllium, beryllium alloys and beryllium compounds.....................1C230

     as powder fuel.................................................ML8.c.5

     as propellant................................................1C111.a.2

     coating technology...............................................2E003

     substrate blanks of..............................................6C004

BHEGA (CAS 17409-41-5)..........................................ML8.f.2

binary precursors to CW agents

     see chemical warfare agents and precursors

binders (chemical)..................................................ML8

biocatalysts.............................................ML22.b.5, ML7.i.1

biological warfare agents

     see also toxicological agents

     animal pathogens...............................................1C352

     bacterial cultures..........................................1C351, 1C354

     cell cultures.......................................ML22.b.4, ML7, ML7.i.2

     containment and handling facilities...................................2B352

     fungi...................................................1C351, 1C354

     handling equipment..............................................2B352

     human pathogens...............................................1C351

     mycoplasmas..................................................1C352

     pathogens, zoonoses and toxins.....................................1C351

     plant pathogens.................................................1C354

     protective clothing and equipment against...................1A004.a.1, 1A004.b.1

     sensors and detectors for.......................................1A004.c.1

     software for determining effects of.................................ML21.b.3

     technology for development and production of.........................ML22.b.3

     virus cultures......................................1C351, 1C354, ML7.i.2

biopolymer technology..........................................ML22.b.4

bioreactors

     see fermenters for pathogenic cultures

biphenylene, in thermoplastic liquid crystal copolymers................1C008.b.1

bis (2,2-dinitropropyl)acetal

     see BDNPA

bis (2,2-dinitropropyl)formal

     see BDNPF

bis (2-chloroethyl) ethylamine (CAS 538-07-8)..........................ML7.b.2

bis (2-chloroethyl) methylamine (CAS 51-75-2).........................ML7.b.2

bis (2-chloroethyl) sulphide (CAS 505-60-2)............................ML7.b.2

bis (2-chloroethylthio) methane (CAS 63869-13-6).......................ML7.b.2

bis (2-chloroethylthioethyl) ether (CAS 63918-89-8)......................ML7.b.2

bis (2-chloroethylthiomethyl) ether (CAS 63918-90-1)....................ML7.b.2

bis (2-chlorovinyl) chloroarsine (CAS 40334-69-8).......................ML7.b.2

bis (2-fluoro-2,2-dinitroethyl) formaldehyde

     see FEFO

bis (2-hydroxyethyl) glycolamide

     see BHEGA

bis (2-methyl aziridinyl) 2-(2-hydroxypropanoxy) propylamino phosphine oxide

     see BOBBA 8

bis (2-methyl aziridinyl) methylamino phosphine oxide (CAS 85068-72-0)

     see methyl BAPO

bisazidomethyloxetane

     see BAMO

bischloromethyloxetane

     see BCMO

bis-dinitrotriazole amine

     see BDNTA

bismaleimides................................................1C008.a.1

bismuth, high-purity...............................................1C229

black powder......................................................ML8

black-out lighting for vehicles.........................................ML6

bladders made from fluoroelastomers.................................1A001

blades for turbine engines

     see gas turbine engines

blast initiation systems

     see detonation equipment

blindness, systems designed to cause.................................ML19

blowers and compressors..........................................1B232

     for aerodynamic separation equipment.............................0B001.d.3

     for gaseous diffusion separators..................................0B001.c.3

     for hydrogen sulphide gas circulation...............................0B004.b.2

     for molecular laser isotope separation equipment......................0B001.h.3

bluetongue virus..............................................1C352.a.3

BNCP (CAS 117412-28-9)..........................................ML8.a.2

BNNII........................................................ML8.a.16

BNO (CAS 9003-18-3).............................................ML8.f.3

boats, military

     see marine vessels, equipment and components

BOBBA 8......................................................ML8.f.11

body armour

     see also protective and decontamination clothing and equipment

..........................................................1A005, ML13

bomb disposal equipment

     see also explosives and explosive devices

...............................................................1A006

bombing computers................................................ML5

bomblets

     see submunitions

bombs

     see also detonation equipment

     see also explosives and explosive devices

................................................................ML4

borides of titanium

     see titanium, titanium alloys and titanium compounds

boron and boron compounds.......................................1C011

     boron carbides (CAS 12069-32-8)........................1B115, 1C011, 1E.c.3

     boron nitrides.............................................1E.c.2, 2E003

     in fibrous form..................................................1C010

     in powder fuel.................................................ML8.c.5

     isotope enriched................................................1C225

boron equivalence................................................0C004

bottom cable systems........6A001.a.2, 6D003.a.1, 6D003.a.2, 6D003.a.3, 6D003.a.4

botulinum toxins..............................................1C351.d.1

Brayton cycle engines, for underwater use...........................8A002.j.1

breathing equipment

     for high altitude parachutists......................................ML10.h.8

     for use in military aircraft...........................................ML10

     full and half suits or hoods.......................................2B352.f.1

     gas masks and components........................................1A004

     self-contained diving apparatus................................8A002, ML17

bremsstrahlung accelerators........................................3A003

bridges and bridge laying vehicles....................................ML17

bromine and bromine compounds

     see also alpha-bromobenzeneacetonitrile

     bromoacetone...................................................ML7

     bromomethylethylketone............................................ML7

Brucella abortus...............................................1C351.c.2

Brucella melitensis.............................................1C351.c.3

Brucella suis..................................................1C351.c.4

brush seals for gas turbine engines...................................9B003

BTTN (CAS 6659-60-5)............................................ML8.e.5

bulk acoustic wave equipment

     see acoustic systems, equipment and components

bullet cups........................................................ML3

bullet proof and resistant materials and clothing

     see protective and decontamination clothing and equipment

bullet-proof tyre casings.............................................ML6

buoyant electric conducting cable.....................................ML4

Burkholderia mallei.............................................1C351.c.8

Burkholderia pseudomallei.......................................1C351.c.9

Burkholderia solanacearum

     see Ralstonia solanacearum

butacene (CAS 125856-62-4)........................................ML8.f.4

butadienenitrileoxide

     see BNO

butanetrioltrinitrate

     see BTTN

butyl 2-chloro-4-fluorophenoxyacetate...............................ML7.b.4

BZ

     see 3-quinuclidinyl benzilate

>>===============================<<

>>C<<

C3I (command, communications, control and intelligence) software........ML21.b.4

CA

     see alpha-bromobenzeneacetonitrile

cables

     see also communications systems

     see also optical fibre, equipment and accessories

     with intrusion detection capabilities................................5A002.a.8

cadmium, cadmium alloys and cadmium compounds

     cadmium telluride.............................................6C002.b.2

     cadmium zinc telluride...................................6C002, 6C002.b.1

calcium and calcium compounds

     calcium fluoride..............................................2A225.a.2

     calcium zirconate.............................................2A225.a.2

     high-purity.....................................................1C227

camera systems, camera equipment, and camera components

     see also optical components and equipment

.........................................................6A003, 6A203

     electronic cameras...................................6A003.a.4, 6A003.a.5

     framing cameras............................6A203.a.1, 6A203.b.1, 6A203.b.3

     high speed cameras..................................6A003.a.1, 6A003.a.2

     imaging cameras...........................................6A003, ML15

     instrumentation cameras..........................................6A003

     low-light-level television camera tubes.................................ML15

     mechanical high speed cameras..................................6A003.a.2

     mechanical rotating mirror cameras..................................6A203

     plug-ins for instrumentation cameras...............................6A003.a.6

     pyroelectric television camera tubes...................................ML15

     radiation hardened...............................................6A203

     rotating mirror cameras...........................................6A203

     scanning cameras............................................6A003.b.2

     streak cameras.............................6A003.a.3, 6A203.a.2, 6A203.b.2

     underwater cameras.............................................8A002

     video cameras.................................6A003.b.1, 6A203, 8A002.d.1

     with focal plane arrays.........................................6A003.b.4

     with solid state sensors.........................................6A003.b.5

cannons, large calibre...............................................ML2

capacitors..............................................3A001.e.2, 3A201

carbides, coating technology........................................2E003

carbines

     see also firearms and firearm components

................................................................ML1

carbon dioxide lasers..............................................6A205

carbon fibre and filamentary materials

     see also fibrous and filamentary materials

...........................................1A002, 1C010, 1C010.e.2, 1C210

carbon graphite materials

     see graphite

carbon monoxide lasers.........................................6A005.d.3

carbon--carbon materials

     see also pyrolised materials and pyrolysis equipment

.........................................................1A102, 1C102

     coating technology...............................................2E003

     for liquid rocket propulsion systems...................................9A006

     one-piece thrust chambers and exit cones..............................9A006

carbonyl chloride

     see phosgene (carbonyl chloride)

carbonyl dichloride.............................................1C450.a.4

carboranes.....................................................ML8.c.3

carboxy/carboxyl-terminated polybutadiene.........................1C111.b.1

cargo parachutes

     see also parachutes

.............................................................ML10.h.2

cartridge links

     see also ammunition and components

................................................................ML3

CAS 100-15-2

     see N-methyl-P-nitroaniline

CAS 10025-67-9

     see sulphur compounds

CAS 10025-87-3

     see phosphorus and phosphorus compounds

CAS 10026-13-8

     see phosphorus and phosphorus compounds

CAS 100-37-8

     see diethylaminoethanol

CAS 10102-03-1

     see dinitrogen pentoxide

CAS 10102-44-0

     see nitrogen dioxide

CAS 102-71-6

     see triethanolamine

CAS 103850-22-2

     see neopentyl[diallyl]oxy, tri[dioctyl]phosphato-titanate

CAS 10544-72-6

     see dinitrogen tetroxide

CAS 10544-73-7

     see dinitrogen trioxide

CAS 10545-99-0

     see sulphur compounds

CAS 1066-50-8

     see ethyl phosphonyl dichloride

CAS 107-07-3

     see 2-chloroethanol

CAS 108-18-9

     see di-isopropylamine

CAS 108-70-3

     see 1,3,5-trichlorobenzene

CAS 110438-25-0

     see neopentyl[diallyl]oxy, tri[dioctyl]phosphato-titanate

CAS 111-22-8

     see triethylene glycol dinitrate

CAS 111-48-8

     see thiodiglycol

CAS 115029-35-1

     see RDX and derivatives

CAS 116-17-6

     see triisopropyl phosphite

CAS 117412-28-9

     see BNCP

CAS 117907-74-1

     see CL-14

CAS 12036-31-6

     see lead and lead compounds

CAS 12069-32-8

     see boron and boron compounds

CAS 121-45-9

     see trimethyl phosphite

CAS 121-82-4

     see RDX and derivatives

CAS 122-52-1

     see triethyl phosphite

CAS 124-40-3

     see dimethylamine

CAS 124782-15-6

     see HBIW

CAS 125735-38-8

     see dinitroazetidine-T-butyl salt

CAS 125856-62-4

     see butacene

CAS 1273-89-8

     see propyl ferrocene

CAS 1274-00-6

     see pentyl ferrocene

CAS 1274-08-4

     see dibutyl ferrocene

CAS 130256-72-3

     see K-55

CAS 130400-13-4

     see NNHT

CAS 1313-82-2

     see sodium and sodium compounds

CAS 1314-80-3

     see triethanolamine

CAS 1333-83-1

     see sodium and sodium compounds

CAS 13465-08-2

     see HAN

CAS 135285-90-4

     see CL-20

CAS 135877-16-6

     see TNAD

CAS 139-87-7

     see ethyldiethanolamine

CAS 140456-78-6

     see ADN

CAS 142173-26-0

     see BCMO

CAS 142868-93-7

     see 1,4-bis (2-chloroethylthio)-N-butane

CAS 142868-94-8

     see 1,5-bis (2-chloroethylthio)-N-pentane

CAS 143178-24-9

     see GAP

CAS 143-33-9

     see sodium and sodium compounds

CAS 143850-71-9

     see hexanitroadamantane

CAS 14450-60-3

     see lead and lead compounds

CAS 1445-76-7

     see O-isopropyl methylphosphonochloridate

CAS 1498-40-4

     see ethyl phosphinyl dichloride

CAS 151-50-8

     see potassium and potassium compounds

...............................................................1C350

CAS 15588-62-2

     see HAP

CAS 15715-41-0

     see diethyl methylphosphonite

CAS 15748-73-9

     see lead and lead compounds

CAS 1614-08-0

     see ADHTDN

CAS 1619-34-7

     see 3-quinuclidinol

CAS 1630-08-6

     see DATB

CAS 16893-85-9

     see sodium and sodium compounds

CAS 17003-79-1

     see FEFO

CAS 17096-47-8

     see NENAs

CAS 17215-44-0

     see DIPAM

CAS 17409-41-5

     see BHEGA

CAS 17607-20-4

     see BAMO

CAS 17702-41-9

     see decaborane

CAS 18433-84-6

     see pentaboranes

CAS 19136-34-6

     see lead and lead compounds

CAS 194486-77-6

     see DDPO

CAS 19624-22-7

     see pentaboranes

CAS 19899-80-0

     see DNAM

CAS 20062-22-0

     see HNS

CAS 20773-28-8

     see dicyclopentyl ferrocene

     see HNF

CAS 20936-32-7

     see lead and lead compounds

CAS 229176-04-9

     see TNP

CAS 2404-03-7

     see diethyl-N,N-dimethylphosphoramidate

CAS 2465-65-8

     see O,O-diethyl phosphorothioate

CAS 25243-36-1

     see TACOT

CAS 257-07-8

     see dibenz-(B,F)-1,4-oxazephine

CAS 2625-76-5

     see 2-chloroethylchloromethylsulphide

CAS 2691-41-0

     see HMX and derivatives

CAS 2698-41-1

     see 2-chlorophenyl methylene propanedinitrile

CAS 27814-48-8

     see PGN

CAS 27978-54-7

     see hydrazine and hydrazine compounds

CAS 298-06-6

     see O,O-diethyl phosphorodithioate

CAS 30003-46-4

     see DBT

CAS 302-01-2

     see hydrazine and hydrazine compounds

CAS 3058-38-6

     see TATB

CAS 3068-00-6

     see 1,2,4-trihydroxybutane

CAS 31904-29-7

     see N-butyl-ferrocene

CAS 3554-74-3

     see 3-hydroxy-1-methylpiperidine

CAS 3563-36-8

     see 1,2-bis (2-chloroethylthio) ethane

CAS 37206-42-1

     see catocene

CAS 3731-38-2

     see 3-quinuclidone

CAS 376-90-9

     see FPF-1

CAS 37836-27-4

     see hydrazine and hydrazine compounds

CAS 38082-89-2

     see PYX

CAS 382-21-8

     see PFIB

CAS 3982-91-0

     see thiophosphoryl chloride

CAS 4000-16-2

     see TAGN

CAS 40334-69-8

     see bis (2-chlorovinyl) chloroarsine

CAS 41378-98-7

     see TAT

CAS 4261-68-1

     see N,N-diisopropyl-(beta)-aminoethyl chloride hydrochloride

CAS 430-78-4

     see ethyl phosphinyl difluoride

CAS 464-07-3

     see pinacolyl alcohol

CAS 479-45-8

     see tetryl

CAS 505-60-2

     see bis (2-chloroethyl) sulphide

CAS 506-59-2

     see dimethylamine hydrochloride

CAS 506-77-4

     see cyanogen chloride

CAS 5108-69-0

     see BDNPA

CAS 51-75-2

     see bis (2-chloroethyl) methylamine

CAS 5213-49-0

     see DNI

CAS 5299-64-9

     see N-nonanoylmorpholine

CAS 53159-39-0

     see TVOPA

CAS 532-27-4

     see 2-chloro-1-phenylethanone

     see phenylacyl chloride

CAS 538-07-8

     see bis (2-chloroethyl) ethylamine

CAS 540-73-8

     see symmetrical dimethyl hydrazine

CAS 5409-42-7

     see 1,4,5,8-tetraazadecalin

CAS 541-25-3

     see 2-chlorovinyldichloroarsine

CAS 55510-03-7

     see TNGU

CAS 55510-04-8

     see DINGU

CAS 555-77-1

     see tris (2-chloroethyl) amine

CAS 55-63-0

     see nitroglycerin

...................................................................0

CAS 556-88-7

     see nitroguanidine

CAS 57-14-7

     see unsymmetrical dimethyl hydrazine

CAS 57-39-6

     see MAPO and derivatives

CAS 57856-11-8

     see O-ethyl-2-di-isopropylaminoethyl methylphosphonite

CAS 578-94-9

     see 10-chloro-5,10-dihydrophenarsazine

CAS 5798-79-8

     see alpha-bromobenzeneacetonitrile

CAS 5842-07-9

     see N,N-diisopropyl-(beta)-aminoethane thiol

CAS 5917-61-3

     see BDNPF

CAS 603-33-8

     see TPB

CAS 60-34-4

     see monomethyl hydrazine

CAS 6163-75-3

     see dimethyl ethylphosphonate

CAS 62320-94-9

     see basic copper salicylate

CAS 637-39-8

     see triethanolamine hydrochloride

CAS 63869-13-6

     see bis (2-chloroethylthio) methane

CAS 63905-10-2

     see 1,3-bis (2-chloroethylthio)-N-propane

CAS 63918-89-8

     see bis (2-chloroethylthioethyl) ether

CAS 63918-90-1

     see bis (2-chloroethylthiomethyl) ether

CAS 6581-06-2

     see 3-quinuclidinyl benzilate

CAS 6659-60-5

     see BTTN

CAS 676-83-5

     see methyl phosphinyl dichloride

CAS 676-97-1

     see methyl phosphonyl dichloride

CAS 676-98-2

     see methylphosphonothioic dichloride

CAS 676-99-3

     see methyl phosphonyl difluoride

     see phosgene (carbonyl chloride)

CAS 677-43-0

     see N,N-dimethyl phosphoramidic dichloride

CAS 683-08-9

     see diethyl methylphosphonate

CAS 68411-07-4

     see lead and lead compounds

CAS 68412-45-3

     see TEPAN

CAS 68412-46-4

     see TEPANOL

CAS 693-21-0

     see diethylene glycol dinitrate

CAS 70247-32-4

     see CP

CAS 70890-46-9

     see DNBT

CAS 7406-61-9

     see 3-nitraza-1,5-pentane diisocyanate

CAS 74-90-8

     see hydrogen and hydrogen compounds

...................................................................0

CAS 753-59-3

     see methyl phosphinyl difluoride

CAS 75393-84-9

     see NTDNA

CAS 75-55-8

     see propyleneimine (2-methylaziridine)

CAS 756-79-6

     see dimethyl methylphosphonate

CAS 75-97-8

     see pinacolone

CAS 76-06-2

     see chloropicrin

CAS 762-04-9

     see diethyl phosphite

CAS 7664-39-3

     see hydrogen and hydrogen compounds

CAS 7681-49-4

     see sodium and sodium compounds

CAS 76-89-1

     see methyl benzilate

CAS 76-93-7

     see benzilic acid

CAS 7719-09-7

     see thionyl chloride

CAS 7719-12-2

     see phosphorus and phosphorus compounds

CAS 77-81-6

     see tabun

...................................................................0

CAS 7784-21-6

     see alane

CAS 7784-34-1

     see arsenic compounds

CAS 7789-23-3

     see potassium and potassium compounds

CAS 7789-29-9

     see potassium and potassium compounds

CAS 7790-98-9

     see AP

CAS 78246-06-7

     see DNAD

CAS 78-38-6

     see diethyl ethylphosphonate

CAS 78-53-5

     see amiton

     see O,O-diethyl S-[2-(diethylamino)ethyl] phosphorothiolate

...................................................................0

CAS 78644-90-3

     see DAAzF

CAS 79-37-8.....................................................1C350

CAS 82486-82-6

     see NENAs

CAS 82486-83-7

     see NENAs

CAS 84051-81-0

     see poly-NMMO

CAS 85068-72-0

     see bis (2-methyl aziridinyl) methylamino phosphine oxide

CAS 85068-73-1

     see NENAs

CAS 85954-06-9

     see NENAs

CAS 868-85-9

     see dimethyl phosphite

CAS 9003-18-3

     see BNO

CAS 90683-29-7

     see AMMO

CAS 932-64-9

     see NTO

CAS 93894-59-8

     see dihexyl ferrocene

CAS 96-79-7

     see N,N-diisopropyl-(beta)-aminoethyl chloride

CAS 96-80-0

     see N,N-diisopropyl-(beta)-amino ethanol

CAS 97096-78-1

     see ADNBF

CAS 97645-24-4

     see TNAZ

CAS 993-13-5

     see methylphosphonic acid

caseless ammunition, weapons using...................................ML1

casting and remelt furnaces

     see furnaces

castings.............................................ML16, ML901, ML902

catalytic burners, for deuterium compound production.................0B004.b.7

cathodes for microwave equipment

     see also vacuum tubes and valves (electronic)

............................................................3A001.b.1

cathodic arc discharge equipment..............................2B005, 2E003

catocene (CAS 37206-42-1).........................................ML8.f.4

cell cultures

     biopolymer technology.............................................ML7

     for use against chemical warfare agents..............................ML7.i.2

     technology for development and production of.........................ML22.b.4

cell-interconnect-coverglass assemblies............................3A001.e.4

cells and batteries (electrical)

     see also power supplies

...............................................................3A102

     fuel cell power systems.........................................8A002.j.3

     primary high energy cells and batteries.............................3A001.e.1

     secondary cells and batteries....................................3A001.e.1

     thermal batteries................................................3A102

cellular mobile phone equipment

     see also communications systems

...............................................................5A002

centralites........................................................ML8

centrifugal balancing machines......................................2B219

centrifugal balancing machines for rotor components

     see rotor assemblies for gas centrifuges

centrifugal fixtures for gyro bearings

     see gyros, gyro components and gyro equipment

centrifugal separators and decanters..................................2B352

centrifugal testing apparatus.........................................ML18

centrifuges, with slip rings..........................................2B122

ceramic materials

     see also composite material components and structures

.........................................................1C007, 1C107

     ceramic--ceramic composite materials................................1C007

     coating technology...............................................2E003

     for gas turbine manufacture........................................9B001

     for radomes....................................................1C107

     in electromagnetic wave absorbers...................................1C001

     in engine systems.............................................9E003.f.1

     in fibrous form..................................................1C010

     in incinerators................................................2B350.i.2

     in pumps....................................................2B350.i.2

     machine tools for removing.........................................2B001

     machine tools for working..........................................2B123

     technology for the production of.....................................1E.c.4

     wet-spinning equipment................................1B001.d.3, 1B101.c.3

cerium sulphide, crucibles coated with.............................2A225.a.2

certification software for information security software

     see information security systems

charges, explosive

     see explosives and explosive devices

chemical exchange isotope separation equipment

     see isotope separation plants, systems, equipment and components

chemical incinerators..............................................2B350

chemical lasers................................................6A005.d.5

chemical manufacturing facilities, equipment and components..............2B350

chemical propulsion systems, kinetic energy weapons.....................ML12

chemical storage tanks and containers................................2B350

     for military use..................................................ML17

     in liquid rocket propulsion systems...................................9A120

     resistant to nitric acid.............................................0B006

chemical toxic agents

     see toxicological agents

chemical vapour deposition equipment.......................1B001.d.2, 2B005

     furnaces......................................................2B105

     metal organic CVD reactors.....................................3B001.a.2

     physical vapour deposition technology................................2E003

     plasma enhanced...............................................3B001

     pulsating...................................................2B005.a.1

     technology for..................................................2E003

chemical warfare agents and precursors

     see also toxicological agents

................................................................ML7

     defoliants....................................................ML7.b.4

     expression vectors for use against chemical warfare agents................ML7.i.2

     incapacitating agents............................................ML7.b.3

     nerve agents..................................................ML7.b.1

     nitrogen mustards..............................................ML7.b.2

     precursors...............................................1C350, 1C450

     protective and decontamination clothing and equipment....1A004.a.3, 1A004.b.3, ML7

     sensor and detector equipment...............................1A004.c.3, ML7

     software for determining effects of.................................ML21.b.3

     sulphur compounds.......................................1C350, ML7.b.2

     tabun.......................................................ML7.b.1

     technology for development and production of.........................ML22.b.3

     vesicant agents................................................ML7.b.2

     virus cultures for use against.......................................ML7.i.2

Chikungunya virus.............................................1C351.a.1

Chlamydia psittaci.............................................1C351.c.5

chlorine and chlorine compounds

     see also O-isopropyl methylphosphonochloridate

................................................................ML7

     chlorates.....................................................ML8.c.7

     chlorine trifluoride........................................1C238, ML8.d.3

     chloro acetone...................................................ML7

     chlorofluorocarbons...........................................1C006.a.2

     chloropicrin.............................................1C450.a.7, ML7

chloropicrin (CAS 76-06-2)...........................................ML7

cholera toxin.................................................1C351.d.13

cholinesterase-inhibiting activity detection.............................2B351

chromates.....................................................ML8.c.7

chromium, chemical handling equipment made with......................2B350

chromosomes

     see genetic elements

CICs

     see cell-interconnect-coverglass assemblies

cinema recording cameras

     see video cameras

cis-bis (5-nitrotetrazolato) tetra amine-cobalt (III) perchlorate

     see BNCP

Cl--

     see chlorine and chlorine compounds

CL-14 (CAS 117907-74-1)..........................................ML8.a.3

CL-20 (CAS 135285-90-4)..........................................ML8.a.4

Clavibacter michiganensis subsp. Sepedonicus......................1C354.b.4

clicker dies, for composite materials..................................1B101

clips............................................................ML1

closed circuit diving apparatus

     see breathing equipment

     see underwater operations equipment

Clostridium botulinum..........................................1C351.c.6

Clostridium perfringens epsilon..................................1C351.c.14

Clostridium perfringens toxins....................................1C351.d.2

clothing and materials

     see protective and decontamination clothing and equipment

CN

     see 2-chloro-1-phenylethanone

CNTD

     see controlled nucleation thermal deposition equipment

coating and processing equipment

     see surface coating and processing materials and equipment

Coccidioides immitis...........................................1C351.e.1

Coccidioides posadasii.........................................1C351.e.2

Cochliobolus miyabeanus.......................................1C354.c.2

coherent optical transmission and detection equipment................5E001.c.2

cold boxes

     see distillation and absorption columns

cold traps and desublimers for UF6 removal

     see also uranium metal, uranium alloys, and uranium compounds

......................................................0B001.d.7, 0B002

cold-cathode tubes...............................................3A228

Colletotrichum coffeanum var. virulans.............................1C354.c.1

Colletotrichum kahawae

     see Colletotrichum coffeanum var. virulans

colour centre lasers...............................................6A005

columbium

     see niobium and niobium alloys

combat aircraft

     see also aircraft and aircraft components

...............................................................ML10

combat parachutes

     see parachutes

combatant vessels and components

     see also marine vessels, equipment and components

     see also submersible vessels, equipment and components

................................................................ML9

combined cycle engines and components..............................9A011

combustion regulation equipment....................................9A118

combustors, technology for development and production of.............9E003.a.2

command, communications, control and intelligence software

     see C3I (command, communications, control and intelligence) software

comminution, alloys made by.....................................1C002.c.2

common channel signalling equipment.....................5B001.b.5, 5E001.c.4

communications systems

     see radio equipment and components

     see telecommunications systems, equipment, components and accessories

     see underwater operations equipment

compasses, gyroscopic

     see gyros, gyro components and gyro equipment

compensation systems............................................6A006

complex programmable logic equipment

     see field programmable gates, logic arrays and interconnects

composite material components and structures

     see also ceramic materials

...................................................1A002, 1C007, 9C110

     coating technology...............................................2E003

     equipment for the production of..........................1B001, 1B201, 2B123

     fibrous and filamentary materials in...................................1C010

     flexible piezoelectric composites..................................6A001.a.2

     for gas turbine engines.........................................9E003.a.3

     for space launch vehicles..........................................9A110

     mirrors constructed from...............................6A004.a.3, 6A004.c.4

     software for the production of.......................................1D002

     space-qualified.................................................9A010

     superconductive composite conductors................................1C005

     tools for removing...............................................2B001

     tubular.......................................................1A202

compound acoustic mounts......................................8A002.o.3

compound rotary tables............................................2B008

compound semiconductor photocathodes, for imaging equipment...........ML15

compound substrates

     see substrate materials for integrated circuits

compressors

     see blowers and compressors

computer controlled tools

     see numerically controlled machine tools

computer-aided-design systems, software for...........................7D003

computers, computer assemblies and computer components

     see also software

     bombing computers...............................................ML5

     fault tolerant...................................................4A003

     for monitoring furnaces...........................................2B227

     for underwater use...............................................8A002

     neural computers................................................4A004

     optical computers...............................................4A004

     radiation hardened............................................4A001.a.2

     ruggedised............................................4A001.a.1, 4A101

     systolic array computers...........................................4A004

     temperature-rated............................................4A001.a.1

condensers

     see heat exchangers and condensers

Congo--Crimean haemorrhagic fever virus...........................1C351.a.2

connection equipment for computers.................................4A003

connectors, optical fibre

     see optical fibre, equipment and accessories

conotoxin....................................................1C351.d.3

construction equipment, for military use................................ML17

contactors

     see switching equipment

containers, chemical

     see chemical storage tanks and containers

containment facilities, biological warfare agents.........................2B352

continuous mixers...........................................1B118, ML18

continuous nitrators...............................................ML18

continuous output accelerometers....................................7A101

continuous-flow fermenters

     see fermenters for pathogenic cultures

contrarotating propeller systems..................................8A002.o.1

control law compensation technology..............................7E004.b.2

controllable-pitch propellers

     see propellers and propfans

controlled atmosphere melting and casting furnaces

     see furnaces

controlled nucleation thermal deposition equipment...................2B005.a.1

convection current converters, manufacturing equipment..................ML18

conversion plant and equipment for uranium

     see uranium metal, uranium alloys, and uranium compounds

conversion tower internals.......................................0B004.b.4

converters (microwave).........................................3A001.b.7

convertors (electrical)

     see frequency changers and generators

cooling equipment for molten uranium

     see uranium metal, uranium alloys, and uranium compounds

cooling systems

     see also cryogenic equipment, accessories and components

     for imaging equipment.............................................ML15

     for isotope separation equipment..................................0B001.h.5

     for nuclear reactors..............................................0A001

     for tritium facilities and plants....................................1B231.b.1

     optical mirrors with............................................6A005.e.1

co-ordinate measuring machines.....................................2B006

copper, copper alloys and copper compounds

     copper salicylate...............................................ML8.f.1

coprocessors

     see digital signal processors and coprocessors

cordless telephone equipment.......................................5A002

correlation--velocity sonar log equipment

     see sonar navigation systems

corrosion-resistant materials........................................0B002

Corynebacterium michiganensis subsp. sepedonicum

     see Clavibacter michiganensis subsp. Sepedonicus

Corynebacterium sepedonicum

     see Clavibacter michiganensis subsp. Sepedonicus

counter-current solvent extractors for nuclear fuel reprocessing............0B006

countermeasure and counter countermeasure equipment..................ML15

     electronic......................................................ML11

     for directed energy weapons........................................ML19

     for negative hydrogen ion beams.....................................ML19

coupled cavity tubes............................................3A001.b.1

couplers

     see optical fibre, equipment and accessories

Coxiella burnetii...............................................1C351.b.1

CP (CAS 70247-32-4).............................................ML8.a.5

CR

     see dibenz-(b,f)-1,4-oxazephine

critically safe tanks for nuclear fuel reprocessing........................0B006

cross flow filtration equipment and components.........................2B352

crossed-field amplifier tubes.....................................3A001.b.1

crucibles

     actinide resistant................................................2A225

     for liquid uranium handling systems................................0B001.g.2

     for plasma separation equipment..................................0B001.i.4

cryogenic distillation towers and cold boxes

     see absorption and distillation columns

cryogenic equipment, accessories and components

     see also cooling systems

...............................................................ML20

     for aerodynamic separation equipment.............................0B001.d.7

     for isotope separation equipment..................................0B001.h.5

     for liquid rocket propulsion systems...................................9A006

     for optical sensors...............................................6A002

     hydrogen-cryogenic distillation columns...............................1B228

     steam sterilisable freeze drying equipment.............................2B352

cryptographic equipment...................................5A002.a.1, ML11

CS

     see [(2-chlorophenyl) methylene] propanedinitrile

CTPB

     see carboxy-terminated polybutadiene

cultures of microorganisms

     see bacterial cultures

     see fungi

     see virus cultures

current injectors..................................................ML19

custom integrated circuits

     see integrated circuits

cutting machines............................................1B101, ML18

CVD

     see chemical vapour deposition equipment

CW agents

     see chemical warfare agents and precursors

cyanginosin

     see microcystin

cyanoethylated polyamines................................ML8.f.20, ML8.f.21

cyanogen bromide..................................................ML7

cyanogen chloride..................................................ML7

cyanogen chloride (CAS 506-77-4).................................1C450.a.5

cyclonite

     see RDX and derivatives

cyclotetramethylenetetranitramine

     see HMX and derivatives

cyclotrimethylenetrinitramine

     see RDX and derivatives

cylinder components using ceramic materials........................9E003.f.1

>>===============================<<

>>D<<

DAAOF.......................................................ML8.a.12

DAAzF (CAS 78644-90-3).........................................ML8.a.12

DACs

     see digital-to-analogue converters

DADE.........................................................ML8.a.6

damage assessment systems...................................ML12, ML19

damage tolerant systems

     see fault tolerant equipment

damping equipment (electromagnetic)..............................5A002.a.4

damping fluids

     see lubricating materials

data acquisition and processing systems

     see also computers, computer assemblies and computer components

     see also sensors and detectors

     see also signal processing equipment

     for aerospace design and testing....................................9B005

     for gas turbine manufacture........................................9B002

data fusion equipment, weapon control systems..........................ML5

data processing security equipment, using ciphering processes.............ML11

data-based reference navigation equipment...........7A003, 7D003.b.3, 7E004.a.6

DATB (CAS 1630-08-6)............................................ML8.a.7

DBRN

     see data-based reference navigation equipment

DBT (CAS 30003-46-4)...........................................ML8.a.32

DDFP.........................................................ML8.a.8

DDPO (CAS 194486-77-6)..........................................ML8.a.9

decaborane (CAS 17702-41-9)......................................ML8.c.3

decanters

     see centrifugal separators and decanters

decontamination equipment..........................................ML7

decoying equipment

     see also explosives and explosive devices

decryption equipment and software

     see cryptographic equipment

deep water fording vehicles

     see amphibious vehicles

deep-hole drilling machines

     see drilling machines

defoliants

     see chemical warfare agents and precursors

deformable mirrors.............................................6A004.a.1

DEGDN

     see diethylene glycol dinitrate

DEHN

     see diethylhydrazine nitrate

dehydration presses...............................................ML18

demolition equipment

     see also explosives and explosive devices

................................................................ML4

dengue fever virus.............................................1C351.a.3

depleted uranium

     see uranium metal, uranium alloys, and uranium compounds

depth charges and components

     see also explosives and explosive devices

................................................................ML4

depth sounders...............................................6A001.a.1

desublimers

     see cold traps and desublimers for UF6 removal

detection and protection equipment

     see protective and decontamination clothing and equipment

     see sensors and detectors

detonation equipment

     see also explosives and explosive devices

...............................................................1A007

     multipoint initiation systems........................................3A232

     non-military....................................................ML909

deuterium compounds.............................................0C003

     concentrators for.............................................0B004.b.8

     manufacturing equipment..............................0B004, 1A225, 1A226

deuterium fluoride lasers........................................6A005.d.5

DEW

     see directed energy weapon systems

DF

     see methyl phosphonyl difluoride

DHTN

     see 3,6-dihydrazino tetrazine nitrate

diacetoxyscirpenol toxin.......................................1C351.d.14

diagnostic equipment, laser beam systems...........................6A005.f.2

dialkyl [methyl, ethyl and propyl (normal and iso)] N,N-dialkyl [methyl, ethyl and propyl (normal and iso)]-phosphoramidates......1C450.b.3

diamino dinitrobenzofuroxan

     see CL-14

diaminoazofurazan

     see DAAzF

diaminoazoxyfurazan

     see DAAOF

diaminohexanitrobiphenyl

     see DIPAM

diaminotrinitrobenzene

     see DATB

diamond materials

     coating technology...............................................2E003

     in optical equipment..............................................6C004

     substrate materials for integrated circuits...............................3E003

diaphragm pumps

     see pumps

diaphragms, made from fluoroelastomers..............................1A001

dibenz-(B,F)-1,4-oxazephine (CAS 257-07-8)...................1A004.a.4, ML7.d.4

dibromotetrafluoroethane, in damping and flotation fluids...............1C006.c.1

dibutyl ferrocene (CAS 1274-08-4).................................1C111.c.6

dicyclohexyl ferrocene..........................................1C111.c.6

dicyclopentyl ferrocene (CAS 20773-28-8)...........................1C111.c.6

dielectric layers, coating technology..................................2E003

dies

     see also rotor assemblies for gas centrifuges

     for bellows.....................................................2B228

     for isostatic presses..............................................2B204

     for superplastic forming and diffusion bonding...........................1B003

     for the production of composite structures..............................1B101

diesel engines

     for submersible vessels..................................8A002.j.2, ML9.b.1

     non-magnetic.................................................ML9.b.3

     technology for development and production of...........................9E003

diethyl ethylphosphonate (CAS 78-38-6)...............................1C350

diethyl ferrocene...............................................1C111.c.6

diethyl methylphosphonate (CAS 683-08-9).............................1C350

diethyl methylphosphonite (CAS 15715-41-0)............................1C350

diethyl phosphite (CAS 762-04-9).....................................1C350

diethylaminoethanol (CAS 100-37-8)..................................1C350

diethyldiphenyl urea................................................ML8

diethylene glycol dinitrate (CAS 693-21-0)...........................1C111.c.5

diethylhydrazine nitrate.........................................1C111.a.4

diethyl-N,N-dimethylphosphoramidate (CAS 2404-03-7)...................1C350

differential analysers..............................................4A101

diffusion bonding technology.........................1B003, 2E003, 9E003.a.7

difluoroaminated analogs of HMX..................................ML8.a.13

difluoroamine..............................................ML8, ML8.e.6

digital array processors and differential analysers

     see digital signal processors and coprocessors

digital cellular radio equipment

     see telecommunications systems, equipment, components and accessories

digital computers

     see computers, computer assemblies and computer components

digital controllers, vibration test systems..............................2B116

digital demodulators...............................................ML11

digital flight controls

     see flight control systems

digital integrated circuits

     see integrated circuits

digital radio equipment

     see radio equipment and components

digital recording equipment

     see recording equipment

digital signal processors and coprocessors

     see signal processing equipment

digital troposcatter-radio communications transmission equipment..........ML11

digital video magnetic tape recorders

     see recording equipment

digital-to-analogue converters............................3A001.a.2, 3A001.a.5

digitisers, waveform

     see waveform digitisers

dihexyl ferrocene (CAS 93894-59-8)................................1C111.c.6

diimido oxalic acid dihydrazine, as propellant........................1C111.a.4

di-isopropylamine (CAS 108-18-9)....................................1C350

dimensional inspection and measuring systems.............2B006, 6B007, 6B008

dimethyl ethylphosphonate (CAS 6163-75-3)............................1C350

dimethyl methylphosphonate (CAS 756-79-6)...........................1C350

dimethyl phosphite (CAS 868-85-9)...................................1C350

dimethylamine (CAS 124-40-3).......................................1C350

dimethylamine hydrochloride (CAS 506-59-2)...........................1C350

dimethylhydrazinium azide, as propellant...........................1C111.a.4

dimethylidiphenyl urea..............................................ML8

DINGU (CAS 55510-04-8)

     see DNGU

dinitroazetidine-t-butyl salt (CAS 125735-38-8).........................ML8.g.2

dinitrobistriazole

     see DNBT

dinitrogen pentoxide (CAS 10102-03-1).............................1C111.a.3

dinitrogen tetroxide (CAS 10544-72-6)..............................1C111.a.3

dinitrogen trioxide (CAS 10544-73-7)...............................1C111.a.3

dinitroglycoluril

     see DINGU

dioctylmaleate.....................................................ML8

DIPAM (CAS 17215-44-0).........................................ML8.a.10

diphenyl methylphosphonate.....................................1C450.b.1

diphosgene.......................................................ML7

dipicramide

     see DIPAM

dipropyl ferrocene.............................................1C111.c.6

direct current power supplies

     see power supplies

direct current propulsion motors and thrusters.......................8A002.a.2

direct view imaging equipment......................................6A002

direct writing equipment for mask and semiconductor making............3B001.f.3

direct-acting hydraulic pressing technology............................2E003

direct-bonded motors..............................................9A007

directed energy weapon systems.....................................ML19

direction finding systems

     see navigation systems, equipment and components

directional solidification casting equipment.......................9B001, 9D004

discharging equipment, explosive

     see explosives and explosive devices

disruptors for explosives disposal....................................1A006

dissolvers for nuclear fuel reprocessing...............................0B006

distillation and absorption columns...................................2B350

divert propulsion (lateral acceleration) systems..........................ML12

diving apparatus, articles and components

     see breathing equipment

     see underwater operations equipment

DM

     see 10-chloro-5,10-dihydrophenarsazine

DMP

     see dimethyl phosphite

DNAD (CAS 78246-06-7)...........................................ML8.d.4

DNAM (CAS 19899-80-0)..........................................ML8.a.31

DNBT (CAS 70890-46-9)..........................................ML8.a.32

DNGU........................................................ML8.a.11

DNI (CAS 5213-49-0).............................................ML8.a.16

Dobrava virus................................................1C351.a.31

Doppler navigation radar equipment.............................6A008, 6A108

Doppler-velocity cable log equipment..............................6A001.a.2

Dothidella ulei

     see Microcyclus ulei

drag parachutes

     see also parachutes

.............................................................ML10.h.3

drilling machines...........................................2B001, 9E003

drogue parachutes

     see also parachutes

.............................................................ML10.h.3

drones

     see unmanned airborne vehicles, systems and components

dye lasers.................................................6A005, 6A205

dynamic signal analysers

     see signal processing equipment

>>===============================<<

>>E<<

eastern equine encephalitis virus..................................1C351.a.4

EB detonators

     see exploding bridge detonators

Ebola virus...................................................1C351.a.5

EB-PVD

     see electron beam equipment

EBW detonators

     see exploding bridge wire detonators

EDDN

     see ethylenediaminedinitrate

EEPROMS

     see electrical erasable programmable read-only memories

EFI detonators

     see exploding foil detonators

elastomer modified cast double base propellants.......................ML8.b.5

electric actuators, technology for development and production of.........7E004.a.5

electric detonators, explosive

     see detonation equipment

electric engines

     see also engines and engine components

     for marine vessels............................................8A002.o.2

     for submersible vehicles.........................................ML9.b.2

electrical erasable programmable read-only memories.................3A001.a.2

electrochemical machining.........................................9E003

electrochemical reduction cells...................................0B001.e.4

electrolytic cells

     for fluorine production............................................1B225

     for lithium isotope separation....................................1B233.b.3

electromagnetic equipment

     see also computers, computer assemblies and computer components

     see also integrated circuits

     see also microwave equipment and components

     see also radio equipment and components

     see also sensors and detectors

     see also signature reduction equipment and materials

...............................................................ML11

     damping equipment...........................................5A002.a.4

     electric field sensors...........................................6D003.b.1

     electrical discharge machines.................................2B001, 9E003

     electrically triggered shutters........................................ML15

     electrically triggered thyristors.......................................3A001

     electroburst equipment............................................1B102

     electron sensing equipment.....................................6A002.a.2

     flight control systems.............................................7A116

     for military use..................................................ML11

     for surveillance and monitoring.......................................ML11

     gradiometers...................................................6A006

     hair type absorbers..............................................1C001

     in electric engines.....................................8A002.o.2, ML9.b.2

     interference protection technology...................................7E102

     isotope separation equipment.................0B001, 0B001.a.9, 0B001.j.4, 1B226

     magnetic bearings..............................0B001.b.7, 2A001, 8A002.o.3

     magnetic field sensors.........................................6D003.b.1

     magnetic metals................................................1C003

     magnetic propulsion systems........................................ML22

     magnetometers........................................6A006, 6D003.b.2

     nuclear precession magnetometers................................6A006.a.2

     power supplies for.............................................0B001.j.6

     propulsion systems...............................................ML12

     pulse protection technology...................................7E102, ML17

     software for....................................................2D002

     three axis magnetic heading sensors.................................7A103

     wave absorbers.................................................1C001

     with superconductive components...........................3A001.e.3, 3A201

electron beam equipment

     see also semiconductor manufacturing equipment

..................................0B001.g.1, 2B005, 2B227, 2E003, 5A001.b.1

electron bombardment mass spectrometers....................0B002.g.3, 3A233

electronic assemblies.............................................3A001

     for boosting processing performance..................................4A003

     for feedback capability............................................2B006

     for reentry vehicles..............................................9A116

     software for development of........................................4D001

     superconductive materials in.......................................3A001

     technology for..................................................4E001

electronic cameras.............................................6A003.a.5

electronic computers and related equipment

     see computers, computer assemblies and computer components

electronic framing cameras......................................6A003.a.4

electronic imaging systems, for underwater use.........................8A002

electronic vacuum tubes and valves

     see vacuum tubes and valves (electronic)

electronically steerable phased array antennae............5A001, 6A008, 6D003.d.2

electro-optical integrated circuits.........................3A001.a.2, 3A001.a.6

electrorheological finishing tools.....................................2B002

electrothermal propulsion systems....................................ML12

EMCDB propellants

     see elastomer modified cast double base propellants

EMP/EMI protection technology

     see electromagnetic equipment

encrypted GPS

     see global navigation satellite systems

encryption equipment and software

     see cryptographic equipment

end caps, for rotor tubes........................................0B001.b.6

end-effectors

     see robot systems

energetic materials....................................ML8, ML8.e.6, ML908

energetic particle beam finishing tools................................2B002

energy storage equipment

     see also capacitors

     see also cells and batteries (electrical)

     see also superconductive materials and equipment

     for directed energy weapons........................................ML19

energy weapons systems

     see directed energy weapon systems

engines and engine components

     see also aero-engines and components

     see also diesel engines

     see also gas turbine engines

     see also marine engines

     see also rocket propulsion systems

................................................................ML9

     Brayton cycle engines..........................................8A002.j.1

     combined cycle engines and components..............................9A011

     cylinder components using ceramic materials.........................9E003.f.1

     direct-bonded motors.............................................9A007

     filament-wound composite motor cases................................9A008

     pulse jet engines................................................9A111

     pumpjet propulsion systems........................................8A002

     ramjet engines and components.....................................9A011

     Rankine cycle engines..........................................8A002.j.1

     reciprocating engines.............................................ML10

     ring-shaped motor stators......................................0B001.b.10

     scramjet engines................................................9A011

     Stirling cycle engines...........................................8A002.j.4

     superconductive propulsion engines...............................8A002.o.2

enriched uranium

     see uranium metal, uranium alloys, and uranium compounds

enrichment plants

     see isotope separation plants, systems, equipment and components

enterohaemorrhagic Escherichia coli........................1C351.c.15, 1C353

environmental chambers...........................................9B106

epitaxial growth equipment

     see also semiconductor manufacturing equipment

...............................................................3B001

epoxy resin impregnated carbon materials........................1A002, 1C010

equine morbillivirus

     see Hendra virus

erbium oxide, crucibles coated with................................2A225.a.2

ERF

     see electrorheological finishing tools

errocene derivatives..............................................ML8.f.4

escape equipment, for use in military aircraft....................ML10, ML10.h.4

Escherichia coli.........................................1C351.c.15, 1C353

ethyl ferrocene................................................1C111.c.6

ethyl iodoacetate...................................................ML7

ethyl phosphinyl dichloride (CAS 1498-40-4)............................1C350

ethyl phosphinyl difluoride (CAS 430-78-4).............................1C350

ethyl phosphonyl dichloride (CAS 1066-50-8)..........................1C3500

ethyl unsymmetrical diphenylurea

     see ethyl-N,N-diphenylurea

ethyldiethanolamine (CAS 139-87-7)..................................1C350

ethylene dihydrazine, as propellant................................1C111.a.4

ethylenediaminedinitrate.............................................ML8

ethylhexylacrylate..................................................ML8

ethyl-N,N-diphenylurea..............................................ML8

ethyl-phosphonothioic dichloride..................................1C450.b.1

ETTs

     see electromagnetic equipment

evaporators

     see isotope separation plants, systems, equipment and components

excimer lasers...........................................6A005, 6A005.d.4

expert systems software

     see also software

................................................2E003, 7D003, 7E004.b.6

exploding bridge detonators......................................1A007.b.1

exploding bridge wire detonators..................................1A007.b.2

exploding foil detonators........................................1A007.b.4

explosive detonator firing sets.......................................1A007

explosives and explosive devices

     see also detonation equipment

     see also fuels and propellants and related equipment

     see also pyrotechnics, pyrotechnic equipment and components

...................................................1C239, ML8, ML8.a.33

     containing energetic materials......................................ML910

     disposal equipment..............................................1A006

     for military use...................................................ML4

     incendiary munitions............................................ML8.c.6

     robot systems for handling...................................2B007, 2B207

expression vectors for use against CW agents..........................ML7.i.2

>>===============================<<

>>F<<

FADEC (full authority digital electronic engine control) software

     see full authority digital electronic controls

FAMAO.......................................................ML8.e.7

fan turbine control systems.....................................9E003.a.10

fast Fourier transform processors........................3A001.a.2, 3A001.a.12

fast reacting ion-exchange resins

     see isotope separation plants, systems, equipment and components

fast switching modules and assemblies

     see switching equipment

fast-exchange liquid-liquid separators......................0B001.e.1, 0B001.e.2

fault tolerant equipment

     computers.....................................................4A003

     gas turbine engines...........................................9E003.a.8

     software for...........................................7D003.d.4, 9D003

     technology for development and production of........................7E004.b.3

FDIA.........................................................ML8.a.16

Fe--

     see iron, iron alloys and iron compounds

feed autoclaves..................................................0B002

feed preparation systems........................................0B001.e.5

FEFO (CAS 17003-79-1)...........................................ML8.e.8

fermenters for pathogenic cultures...................................2B352

ferries..........................................................ML17

ferrocene and ferrocene derivatives.........................1C111.c.6, ML8.f.4

ferrosilicon, in pumps...........................................2B350.i.2

fibre 'lasers', in optical components...................................6A005

fibre optic cable

     see optical fibre, equipment and accessories

fibrous and filamentary materials

     see also graphite

.........................................................1C010, 1C210

     aromatic polyamide fibres............................................1E

     components made from...........................................1A002

     equipment for the production of.....................................1B001

     in the form of tubes..............................................1A202

     inorganic......................................................1C010

field engineer equipment, for military use...............................ML17

field generators, for military use......................................ML17

field programmable gates, logic arrays and interconnects...............3A001.a.7

field test equipment, weapon control systems............................ML5

filament winding equipment and software........................1B001, 1B201

filamentary materials

     see fibrous and filamentary materials

filament-wound composite motor cases...............................9A008

filling equipment, remotely controlled and operated

     see remotely operated equipment

film processing equipment

     see also camera systems, camera equipment, and camera components

...............................................................ML15

filters

     see Kalman filtering software

     see tunable band-pass filters

fingers for surface effect vessels.....................................8A002

finishing machines

     see machine tool equipment, components and assemblies

fire bombs and components

     see incendiary munitions, fuels for use in

fire control and warning equipment and related systems

     see weapons control systems

firearms and firearm components

     see also ammunition and components

     see also smooth-bore weapons

................................................................ML1

     high velocity kinetic energy weapon systems............................ML12

     non-military....................................................ML901

     technology for development and production of.........................ML22.b.2

     training equipment...............................................ML14

firing sets

     see detonation equipment

first generation image intensifier tubes

     see image processing and enhancement equipment

flame throwers..............................................ML2, ML8.c.6

flares for aircraft missile protection....................................ML4

flash memories................................................3A001.a.2

flash suppressors............................................ML1, ML904

flash x-ray generators.............................................3A201

flexible piezoelectric composites in hydrophones.....................6A001.a.2

flexible rotor centrifugal balancing machines

     see rotor assemblies for gas centrifuges

flight control systems.............................................7E104

     fluid injection thrust vector control systems.............................9A008

     fly-by-light control systems..............................7D003.d.3, 7E004.c.1

     fly-by-wire control systems..............................7D003.d.3, 7E004.c.1

     for unmanned airborne vehicles...................................ML10.c.3

     full authority digital electronic engine controls...........................9D003

     hydraulic......................................................7A116

     integrated flight instrument systems..........................7A103, 7D003.d.2

     optical sensor array technology...................................7E004.a.6

     software for.................................................7D003.d.1

     space-qualified.................................................7A116

     technology for..................................................7E004

     total control systems...........................................7E004.b.5

flightweight dewars, for liquid rocket propulsion systems..................9A006

flotation fluids

     see lubricating materials

flow-environments

     simulators and components for......................................9B005

     software for....................................................9D004

     transducers for testing............................................9B008

flow-forming machines

     see also machine tool equipment, components and assemblies

...................................................2B009, 2B109, 2B209

fluid energy mills............................................1B119, ML18

fluid injection thrust vector control systems............................9A008

fluid jet finishing tools.............................................2B002

fluorine and fluorine compounds....................................ML8.d.3

     as propellants...............................................1C111.a.3

     components made from...........................................1A001

     electrolysis cells for the production of.................................1B225

     fluorinated polyimides............................................1C009

     fluorinated silicone fluids........................................1C006.b.2

     fluorinating equipment.........................................0B001.h.4

     fluoroelastomers.............................................1A001, 1E

     fluorophosphate glass............................................6C004

     fluoropolymers..................................................2B350

     in cooling fluids................................1C006, 1C006.d.1, 1C006.d.4

     unprocessed...................................................1C009

fluxgate technology............................................6A006.a.3

fly cutting machines............................................2B001.b.4

fly-by-light and fly-by-wire control systems..................7D003.d.3, 7E004.c.1

foam structures..........................................6A004.a.3, 8C001

focal plane arrays.....................................6A002.a.3, 6A002.c.2

     imaging cameras with..........................................6A003.b.4

     space qualified.................................................6A002

fogging systems..................................................9A350

fonofos......................................................1C450.b.1

foot and mouth disease virus.....................................1C352.a.4

forgings.............................................ML16, ML901, ML902

FOX7

     see DADE

FPF-1 (CAS 376-90-9).............................................ML8.e.9

FPF-3........................................................ML8.e.10

FPG/LAs

     see field programmable gates, logic arrays and interconnects

framing cameras

     see also camera systems, camera equipment, and camera components

...........................................6A203.a.1, 6A203.b.1, 6A203.b.3

framing tubes.................................................6A203.b.4

Francisella tularensis...........................................1C351.c.7

freeze drying equipment

     see cryogenic equipment, accessories and components

frequency agility radar technology (frequency hopping)...5A001.b.3, 5A002.a.5, ML11

frequency analysers

     see signal processing equipment

frequency changers and generators.........................0B001.b.13, 3A225

frequency extenders, mixers and converters

     see microwave equipment and components

frequency signal generators

     see signal processing equipment

frequency standards

     see atomic frequency standards

fuel cell air independent power systems

     see air independent power systems

fuel cell power systems, for underwater use

     see cells and batteries (electrical)

fuels and propellants and related equipment........................1C111, ML8

     bonding systems................................................9A008

     equipment for the production of.....................................1B115

     for aircraft....................................................ML8.c.1

     for directed energy weapons........................................ML19

     for nuclear reactors........................................0B005, 0B006

     fuel injection systems..........................................9E003.f.3

     liquid propellant charges............................................ML2

     metal powder fuels..........................1B102, 1C111.a.2, ML18, ML8.c.5

     pressure refuellers...............................................ML10

     propellant injectors...............................................9A006

     remotely operated shredding equipment...............................0B006

     storage systems...........................................9A006, 9A120

     thickeners for.................................................ML8.c.6

     UN classified...........................................ML8.b.1, ML8.b.2

full authority digital electronic controls.......................9D003, 9E003.a.9

fully automatic smooth-bore weapons..................................ML1

functional testing equipment for integrated circuits

     see integrated circuits

fungi.....................................................1C351, 1C354

furazans......................................................ML8.a.12

furnaces

     arc remelt furnaces..............................................2B227

     casting furnaces................................................2B227

     controlled atmosphere induction furnaces and components............2B226, 2B227

     electron beam melting furnaces.....................................2B227

     monitoring systems..............................................2B227

     plasma furnaces................................................2B227

     power supplies for...............................................2B226

fused silica, in optical materials......................................6C004

fuze setting equipment for smooth-bore weapons.........................ML3

>>===============================<<

>>G<<

Ga--

     see gallium and gallium compounds

GA (tabun)

     see tabun

Galileo navigation system

     see global navigation satellite systems

gallium and gallium compounds

     in photocathodes.............................................6A002.a.2

     subtrate materials for integrated circuits....................3C001, 3C005, 3C006

gamma-chloroacetophenone

     see 2-chloro-1-phenylethanone

     see phenylacyl chloride

GAP (CAS 143178-24-9)..........................................ML8.e.11

gas atomisation, alloys made by...................................1C002.c.2

gas blowers

     see blowers and compressors

gas centrifuges and components

     see also isotope separation plants, systems, equipment and components

     see also rotor assemblies for gas centrifuges

.........................................................0B001, 2B228

gas generators...........................................9E003.a.10, ML2

gas guns.............................................2B232, 9B005, ML12

gas krytron tubes.................................................3A228

gas masks and components........................................1A004

gas monitoring systems

     see toxicological agents

gas tunnels.....................................................9B005

gas turbine engines

     see also aero-engines and components

     see also engines and engine components

     see also rotor assemblies for gas centrifuges

     blade manufacturing equipment.....................................9B001

     clearance control software.........................................9D004

     components of..................................................9A003

     fault tolerant.................................................9E003.a.8

     manufacturing equipment.........................9B002, 9B003, 9B004, 9B009

     rotor technology.................................................9E003

     software for design, manufacturing and operation........................9D004

     technology for development and production.............................9E003

     tip shroud castings..............................9B001, 9E003.a.4, 9E003.a.5

     vanes for.....................................9B001, 9E003.a.4, 9E003.a.5

gaseous diffusion barriers and housings..............0B001.c.1, 0B001.c.2, 0C005

gaseous diffusion separators

     see isotope separation plants, systems, equipment and components

gases, toxic

     see chemical warfare agents and precursors

     see riot control agents

gaskets, made from fluoroelastomers.................................1A001

gate silicon intensifier target videcon tubes..........................6A203.b.4

gate turn-off thyristors.............................................3A001

GB

     see sarin

GD

     see soman

GDMS

     see glow discharge mass spectrometers

gear manufacturing machine tools....................................2B003

genetic elements.................................................1C353

genetically modified organisms

     see also biological warfare agents

...............................................................1C353

genomes

     see genetic elements

germanium subtrate materials for integrated circuits.....................3C001

gimbals for optical control equipment..............................6A004.d.3

glass and glass-based materials

     see also fibrous and filamentary materials

     see also optical fibre, equipment and accessories

     see also silicon and silicon compounds

     chemical handling equipment made with...............................2B350

     coating technology...............................................2E003

     fibrous and filamentary materials....................................1C210

     in optical materials...............................................6C004

     radiation shielding windows........................................1A227

glass lasers.............................................6A005.d.6, 6A205

global navigation satellite systems..............................7A003, 7A005

     jamming equipment...............................................ML11

     receiving equipment..............................................7A105

     software using...............................................7D003.b.2

GLONASS

     see global navigation satellite systems

glow discharge mass spectrometers..................................3A233

glyceroltrinitrate...................................................ML8

glycidylazide polymer

     see GAP

GNSS

     see global navigation satellite systems

goat pox virus.................................................1C352.a.5

GPS (global positioning system) equipment and components

     see global navigation satellite systems

graphite.............................................2B350.d.3, 2B350.e.4

     controlled materials..............................................1C107

     distillation and absorption columns made with........................2B350.e.4

     heat exchangers and condensers made with.........................2B350.d.3

     nuclear grade..................................................0C004

gravimeters

     see gravity meters and components

gravity gradiometers, components and software.............6A007, 6A107, 6D003

gravity meters and components....................6A007, 6A107, 6B007, 6D003

grenades and components

     see also explosives and explosive devices

................................................................ML4

grinding machines

     see also gear manufacturing machine tools

.........................................................2B001, 2B123

ground control equipment

     see flight control systems

     see launch and launch support equipment

ground vehicles

     see land vehicles and components

GTOs

     see gate turn-off thyristors

guanidine nitrate.................................................1C011

guidance equipment

     see navigation systems, equipment and components

guidance sets for missiles....................................7A117, 7D103

guns and components

     see also cannons, large calibre

     see also firearms and firearm components

     see also smooth-bore weapons

................................................................ML2

     armed vehicles...................................................ML6

     gun laying equipment..............................................ML5

     gun mountings...................................................ML1

     high-velocity gun systems.........................................2B232

gyros, gyro components and gyro equipment................7A002, 7A103, 7B003

     calibration equipment.............................................7B002

     for missiles....................................................7A102

     gyro-astro compasses......................................7A004, 7A104

     gyrostabilisers..................................................7A103

>>===============================<<

>>H<<

hafnium, hafnium alloys and hafnium compounds.......................1C231

     crucibles coated with..........................................2A225.a.2

     hafnium fluoride.................................................6C004

     in particle form.................................................1C011

hair type absorbers...............................................1C001

HAN (CAS 13465-08-2)............................................ML8.d.5

Hantaan virus.................................................1C351.a.6

HAP (CAS 15588-62-2)............................................ML8.d.6

harmonic mixers...............................................3A001.b.7

HBIW (CAS 124782-15-6)..........................................ML8.g.3

HBTs

     see hetero-bipolar transistor technology

He3

     see helium-3, mixtures and products containing

heading sensors

     see also hydrophones

     see also navigation systems, equipment and components

     see also sensors and detectors

............................................................6A001.a.2

head-up displays......................................7D003.d.7, 7E004.a.3

heat exchangers and condensers....................................2B350

     for aerodynamic separation equipment.....................0B001.d.4, 0B001.d.7

     for gaseous diffusion separators..................................0B001.c.5

     for molecular laser separation equipment............................0B001.h.5

     for nuclear reactors..............................................0A001

heat shield and heat sink components.................................9A116

heat-rated equipment

     see temperature-rated equipment

heavy water

     see deuterium compounds

HEHN

     see 2-hydroxyethylhydrazine nitrate

helicopters

     power transmission systems........................................9E003

     rotor blades for...............................................7E004.c.3

     technology for..................................................7E004

helium-3, mixtures and products containing............................1C232

helix tubes...................................................3A001.b.1

helmets

     see protective and decontamination clothing and equipment

Helminthosporium oryzae

     see Cochliobolus miyabeanus

hematite

     see iron, iron alloys and iron compounds

hemishell inspection tools..........................................2B206

hemostats

     see fermenters for pathogenic cultures

HEMTs

     see high electron mobility transistor technology

Hendra virus.................................................1C351.a.29

hetero-bipolar transistor technology..................................3E003

hetero-epitaxial materials...........................................3C001

hetero-structure semiconductor technology............................3E003

hexabenzylhexaazaisowurtzitane

     see HBIW

hexahydro-1,3,5-trinitro-1,3,5-triazine

     see RDX and derivatives

hexanitroadamantane (CAS 143850-71-9)

     see HNAD

hexanitrodiphenylamine.............................................ML8

hexanitrohexaazaisowurtzitane

     see CL-20

hexanitrostilbene

     see HNS

hexogen

     see RDX and derivatives

hexogene

     see RDX and derivatives

high explosives

     see explosives and explosive devices

high-altitude equipment, robot systems................................2B007

high-current pulse generators.......................................3A229

high-electron mobility transistor technology............................3E003

high-energy equipment............................................3A001

high-energy fuels

     see aircraft fuels

     see fuels and propellants and related equipment

high-energy storage capacitors

     see capacitors

high-power direct current power supplies........................3A226, 3A227

high-power electron beam guns

     see electron beam equipment

high-pressure thrust chambers and nozzles

     see rocket propulsion systems

high-pressure turbo pumps.........................................9A006

high-speed cameras

     see camera systems, camera equipment, and camera components

high-speed pulse generators

     see pulse generators

high-velocity gun systems

     see firearms and firearm components

HMX and derivatives (CAS 2691-41-0)...............................ML8.a.13

HN1/2/3

     see nitrogen and nitrogen compounds

HNAD........................................................ML8.a.14

HNF (CAS 20773-28-8)............................................ML8.d.7

HNIW

     see CL-20

HNS (CAS 20062-22-0)...........................................ML8.a.15

hog cholera virus

     see swine fever virus

holding and storage vessels

     see chemical storage tanks and containers

hollow cylinder centrifugal balancing machines

     see rotor assemblies for gas centrifuges

hollow fan blades.............................................9E003.a.11

homing seeker systems.............................................ML12

honing machines

     see machine tool equipment, components and assemblies

hot embossing tools............................................3B001.f.2

hot isostatic densification technology.................................2E003

hot isostatic presses...................................2B004, 2B104, 2B204

hot melt prepeg production equipment................................1B001

hot-shot tunnels..................................................9B005

housings for isotope separation equipment..0B001.d.5, 0B001.g.4, 0B001.i.6, 0B001.j.3

hovercraft

     see surface-effect vehicles

howitzers.........................................................ML2

HT-2 toxin...................................................1C351.d.16

HTPB...............................................1C111.b.2, ML8.e.12

hub assemblies for marine power transmission systems................8A002.o.2

hull penetrators and connectors.................................8A002, ML9

human pathogens................................................1C351

hybrid computers.................................................4A101

hybrid inertial navigation systems....................................7A003

hybrid integrated circuits...........................................3A001

hybrid rocket propulsion systems

     see rocket propulsion systems

hydraulic flight control systems......................................7A116

hydraulic fluids..................................................1C006

hydraulic stretch-forming machine technology..........................2E003

hydrazine and hydrazine compounds (CAS 37836-27-4, CAS 302-01-2, CAS 27978-54-7)......1C111.a.4, ML8

hydrides, subtrate materials for integrated circuits.......................3C004

hydrocarbon fuels

     see fuels and propellants and related equipment

hydrofoil vessels and components..............................8A001, 8A002

hydrogen and hydrogen compounds

     see also deuterium compounds

     see also tritium

     hydrogen cyanide (hydrocyanic acid, CAS 74-90-8)................1C450.a.6, ML7

     hydrogen fluoride (CAS 7664-39-3)...................................1C350

     water-hydrogen sulphide exchange plants.............0B004.a.1, 0B004.b.1, 1B229

hydrogen cryogenic distillation columns...............................1B228

hydrogen fluoride lasers.........................................6A005.d.5

hydrogen isotope storage and purification systems

     see isotope separation plants, systems, equipment and components

hydrophones

     see also sensors and detectors

     see also underwater operations equipment

...........................................6A001.a.2, 6D003.a.1, 6D003.a.2

hydroxyl terminated polybutadiene

     see HTPB

hydroxylammonium nitrate

     see HAN

hydroxylammonium perchlorate

     see HAP

hydroxy-terminated polybutadiene

     see HTPB

>>===============================<<

>>I<<

ICPMS

     see inductively coupled plasma mass spectrometers

IEDs

     see improvised explosive devices

IGCTs

     see integrated gate commutated thyristors

igniters

     see detonation equipment

image processing and enhancement equipment....................4A003, ML15

     for underwater use............................................8A002.d.1

     image intensifiers.......................6A002.a.2, 6A002.c.1, 6A003.b.3, ML15

     infrared imaging equipment.........................................ML15

     solid-state imaging equipment...........................6A003.b.5, 6A203.b.4

imaging cameras

     see also camera systems, camera equipment, and camera components

...............................................................6A003

imaging sensor equipment

     see sensors and detectors

imidazoles....................................................ML8.a.16

impellers for use in reaction vessels..................................2B350

imprint lithography equipment.................3B001, 3B001.f.1, 3B001.f.2, 3C002

improvised explosive devices.........................................ML4

incapacitating agents

     see chemical warfare agents and precursors

incendiary munitions, fuels for use in................................ML8.c.6

incinerators for destroying chemicals.................................2B350

independent air power systems

     see air independent power systems

indicator heads for balancing machines...............................2B119

indium substrate materials....................................3C001, 3C003

induction coil magnetometers

     see also electromagnetic equipment

............................................................6A006.a.4

induction furnaces

     see furnaces

inductively coupled plasma mass spectrometers........................3A233

inertial navigation systems, equipment and components

     see also navigation systems, equipment and components

................................................7A003, 7D002, 7E004.a.4

inflatable membrane finishing tools...................................2B002

information security systems

     see also cryptographic equipment

     see also jamming equipment

.........................................................4D003, 5A002

infrared absorption analysers.....................................0B004.b.6

infrared imaging equipment..........................................ML15

infrared sensors and detectors

     see also sensors and detectors

............................................................6A002.a.3

inhibited red fuming nitric acid....................................1C111.a.3

initiation systems

     see detonation equipment

inorganic fibres and filamentary materials

     see fibrous and filamentary materials

inorganic overlays

     see surface coating and processing materials and equipment

INS

     see inertial navigation systems, equipment and components

inspection equipment

     see test, inspection and production equipment

inspection equipment for hemishells

     see dimensional inspection and measuring systems

instruction generators for machine tools

     see machine tool equipment, components and assemblies

instrumentation cameras...........................................6A003

insulation in rockets.........................................9A008, 9C108

integrated circuits

     see also semiconductor manufacturing equipment

     see also substrate materials for integrated circuits

...............................................................3A001

     electro-optical.......................................3A001.a.2, 3A001.a.6

     monolithic.............................................3A001, 3A001.b.2

     neural network integrated circuits.................................3A001.a.9

     optical integrated circuits..................................3A001, 3A001.a.6

     radiation hardened............................................3A001.a.1

     storage integrated circuits.......................................3A001.a.4

integrated flight instrument systems

     see flight control systems

integrated gate commutated thyristors................................3A001

integrated navigation systems

     see also navigation systems, equipment and components

.........................................................7A103, 7D102

interconnect equipment

     see computers, computer assemblies and computer components

interferometers..........................................2B006.b.1, 6A225

interlacing machines..............................................1B001

interstages, usable in missiles.......................................9A117

intrinsic magnetic gradiometers

     see electromagnetic equipment

intrinsically conductive polymers....................................1C001

inverters (electrical)

     see frequency changers and generators

iodo acetone......................................................ML7

ion exchange separators

     see also isotope separation plants, systems, equipment and components

.................................................0B001, 0B001.a.5, 0B006

ion implantation equipment..............................2B005, 2E003, 3B001

ion plating technology.......................................2B005, 2E003

ion sources

     see mass spectrometers and ion sources

IRFNA

     see inhibited red fuming nitric acid

iron, iron alloys and iron compounds

     see also steels

     as powder fuels................................................ML8.c.5

     ferrocene carboxylic acids.........................................ML8.f.4

     ferrocene derivatives..........................................1C111.c.6

     ferrosilicon, in pumps...........................................2B350.i.2

     superfine iron oxide............................................ML8.f.19

isolators for biological agents.....................................2B352.f.2

isostatic presses

     see hot isostatic presses

isotope separation plants, systems, equipment and components.........0B001.a.3

     aerodynamic separators...........................................0B001

     atomic vapour laser separators...................................0B001.a.6

     chemical exchange separators...................................0B001.a.4

     electromagnetic components.............................0B001.j.4, 0B001.j.6

     fast reacting ion-exchange resins..................................0B001.f.1

     for lithium isotope separation....................................1B233.b.4

     gas centrifuge separators.......................................0B001.a.1

     gaseous diffusion separators....................................0B001.a.2

     hydrogen isotope storage and purification systems...............1A225, 1B231.b.2

     ion exchange separators..................................0B001.a.5, 0B006

     liquefaction stations..............................................0B002

     lithium separation..........................................1B233, 1C233

     molecular laser isotope separation equipment..................0B001, 0B001.a.7

     plasma separators......................................0B001, 0B001.a.8

     product and tails collector systems..........0B001.g.3, 0B001.h.2, 0B001.i.5, 0B002

     separation nozzle units................................0B001.d.1, 0B001.d.7

     supersonic expansion nozzles....................................0B001.h.1

     using corrosion-resistant materials...................................0B002

     vortex tubes................................0B001.d.1, 0B001.d.2, 0B001.d.7

>>===============================<<

>>J<<

jamming equipment

     see also explosives and explosive devices

     for global navigation satellite systems..................................ML11

     for telecommunications systems.....................................5A001

Japanese encephalitis virus.....................................1C351.a.20

jet engines and components

     see aero-engines and components

jig boring machines............................................2B001.b.3

Joule--Thomson self-regulating minicoolers.........................6A002.d.2

Junin virus...................................................1C351.a.7

>>===============================<<

>>K<<

K-55 (CAS 130256-72-3)..........................................ML8.a.13

K-6

     see RDX and derivatives

Kalman filtering software...........................................7D102

Kerr cells....................................................6A203.b.4

keto-bicyclic HMX

     see K-55

keto-RDX

     see RDX and derivatives

key precursors to chemical warfare agents

     see chemical warfare agents and precursors

keyloader equipment

     see also cryptographic equipment

...............................................................ML11

KR3538

     see titanium, titanium alloys and titanium compounds

krytron tubes....................................................3A228

     vacuum tubes and valves (electronic).................................3A228

Kyasanur Forest virus.........................................1C351.a.21

>>===============================<<

>>L<<

laminates

     see composite material components and structures

land vehicles and components........................................ML6

     bridges and bridge laying vehicles....................................ML17

     launch vehicles...........................................9A110, 9B116

     mobile repair shops and related equipment..............................ML17

     recovery vehicles..............................................ML10.h.5

     remotely operated bomb disposal units................................1A006

     surface-effect vehicles............................................8A001

landing deceleration parachutes

     see also parachutes

.............................................................ML10.h.6

laser beam systems.........................................6A005, 6A205

     coating and processing equipment...................................2E003

     diagnostic equipment..........................................6A005.f.2

     for communications...................................5E001.b.2, 5E001.c.2

     for directed energy weapons........................................ML19

     for isotope separation.............................................0B001

     for light detection and ranging equipment (LIDAR)........................6A008

     for measuring instruments and systems................................2B006

     for submersible vehicles........................................8A002.d.2

     for underwater communications...................................5A001.b.1

     for vapour deposition systems....................................2B005.c.1

     in radar systems...........................................6A008, 6A108

     protective military................................................ML17

     pulsed lasers...................................................ML19

     ring laser gyros.................................................7B002

     super high-powered..............................................6E003

     synthetic crystalline host material....................................6C005

Lassa fever virus..............................................1C351.a.8

launch and launch support equipment.................................9A115

     for kinetic energy weapons.........................................ML12

     for unmanned airborne vehicles...................................ML10.c.2

     launch vehicles................................9A010, 9A110, 9A115, 9B116

     projectile launchers................................................ML2

     software for..............................................9D103, 9D105

     technology for..................................................9E012

laying equipment

     see explosives and explosive devices

lead and lead compounds.....................................ML8, ML8.f.5

lewisites.......................................................ML7.b.2

libraries

     see parametric technical databases (libraries)

LICA 12

     see neopentyl[diallyl]oxy, tri[dioctyl]phosphato-titanate

LIDAR

     see light detection and ranging equipment (LIDAR)

lift fans for surface effect vessels....................................8A002

light detection and ranging equipment (LIDAR)..........................6A008

light gas gun systems

     see gas guns

light triggering thyristors...........................................3A001

lighter than air vehicles

     see aircraft and aircraft components

lighting systems, for underwater use..................................8A002

linear accelerometers........................................7A001, 7A101

linear and angular displacement measuring instruments

     see dimensional inspection and measuring systems

linear focal plane arrays

     see focal plane arrays

linear position feedback units

     see also sensors and detectors

...............................................................2B008

linear voltage differential transformer systems.......................2B006.b.1

liquefaction stations...............................................0B002

liquid fuels and propellants

     see fuels and propellants and related equipment

liquid lasers.....................................................6A005

liquid metal handling systems

     see also crucibles

.............................................................0B001.i.4

liquid oxidisers

     see oxidisers

liquid oxygen converters............................................ML10

liquid rocket propulsion systems

     see rocket propulsion systems

liquid uranium handling systems

     see uranium metal, uranium alloys, and uranium compounds

lithium isotope separation facilities

     see isotope separation plants, systems, equipment and components

lithography equipment, for wafer processing............................3B001

LNF

     see butyl 2-chloro-4-fluorophenoxyacetate

location and object detection systems

     see sensors and detectors

     see underwater operations equipment

logic processors and assemblies

     see also field programmable gates, logic arrays and interconnects

...............................................................4A003

Louping ill virus..............................................1C351.a.22

low-light-level television camera tubes.................................ML15

LTTs

     see light triggering thyristors

lubricating materials..............................................1C006

lumpy skin disease virus.......................................1C352.a.16

lymphocytic choriomeningitis virus................................1C351.a.9

lyssa virus...................................................1C352.a.8

>>===============================<<

>>M<<

machine guns and machine pistols

     see also firearms and firearm components

................................................................ML1

machine tool equipment, components and assemblies

     see also numerically controlled machine tools

     see also rotor assemblies for gas centrifuges

     assemblies and units.............................................2B008

     for removing materials............................................2B001

     for superplastic forming and diffusion bonding...........................1B003

     for the production of composite structures..............................1B101

     numerically controlled............................................2B001

Machupo virus...............................................1C351.a.10

magazines (ammunition)

     see ammunition and components

Magnaporthe grisea............................................1C354.c.6

magnesium, magnesium alloys and magnesium compounds....1C002.b.5, 1C002.c.1

     as propellant................................................1C111.a.2

     high-purity.....................................................1C228

     in particle form.................................................1C011

     in powder fuel.................................................ML8.c.5

     magnesium oxide.............................................2A225.a.2

magnetic equipment

     see electromagnetic equipment

magnetorheological finishing tools...................................2B002

magnetostrictive alloys............................................1C003

mandrels

     for bellows.....................................................2B228

     for composite structures...........................................1B101

     for filament winding machines.......................................1B201

     for forming rotors................................................2B209

manganin gauges.................................................6A226

manipulative equipment

     for nuclear reactors..............................................0A001

     for underwater use...............................................8A002

manned submersible vehicles

     see submersible vessels, equipment and components

manufacturing equipment

     see machine tool equipment, components and assemblies

MAPO and derivatives (CAS 57-39-6)................................ML8.f.11

maraging steels............................................1C116, 1C216

Marburg virus................................................1C351.a.11

marine acoustic systems

     see acoustic systems, equipment and components

marine engines

     see propellers and propfans

marine vessels, equipment and components

     see also propellers and propfans

     see also submersible vessels, equipment and components

..................................................................8A

     acoustic systems, equipment and components..........................6A001

     amphibious vehicles...............................................ML6

     ferries.........................................................ML17

     marine engines.........................................8A002.o.2, 9A002

     pumpjet propulsion systems........................................8A002

     stabilisers for...................................................8A002

masks (facial)

     see protective and decontamination clothing and equipment

masks for integrated circuits

     see semiconductor manufacturing equipment

mass spectrometers and ion sources.................................3A233

     in isotope separators..............0B001.j.2, 0B002, 0B002.g.2, 0B002.g.4, 1B226

     microfluorination ion sources.......................................3A233

     molecular beam mass spectrometers.................................3A233

materials, for aerospace design and testing...............................9C

McAlX, coating technology..........................................2E003

MCTs

     see MOS controlled thyristors

measuring instruments and systems

     see dimensional inspection and measuring systems

     see sensors and detectors

mechanical alloying, alloys made by...............................1C002.c.2

mechanical cameras

     see camera systems, camera equipment, and camera components

melt extraction and spinning, alloys made by................1C002.c.2, 1C002.d.3

melting and casting furnaces

     see furnaces

mercury amalgam pumps........................................1B233.b.2

mercury cadmium telluride.......................................6C002.b.3

metal alloys

     see alloys

metal coated fibre preforms

     see fibrous and filamentary materials

metal organic chemical vapour deposition reactors

     see chemical vapour deposition equipment

metal powder fuels...............................................ML8.c.5

     as propellants...............................................1C111.a.2

     manufacturing equipment.....................................1B102, ML18

metal vessels for nuclear reactors....................................0A001

metal working process tools, die and fixture technology

     see machine tool equipment, components and assemblies

metallurgical melting and casting furnaces

     see furnaces

metals

     see also name of metal, e.g. aluminium

     in particle form.................................................1C011

     machine tools for removing.........................................2B001

methyl BAPO..................................................ML8.f.12

methyl benzilate (CAS 76-89-1)......................................1C350

methyl phosphinyl dichloride (CAS 676-83-5)...........................1C350

methyl phosphinyl difluoride (CAS 753-59-3)............................1C350

methyl phosphonyl dichloride (CAS 676-97-1)...........................1C350

methyl phosphonyl difluoride (CAS 676-99-3)....................1C350, ML7.c.1

methyl unsymmetrical diphenylurea

     see methyl-N,N-diphenylurea

methyldiethanolamine..........................................1C450.b.8

methylethyldiphenyl  urea............................................ML8

methylhydrazine nitrate.........................................1C111.a.4

methyl-N,N-diphenylurea.............................................ML8

methylphosphonic acid (CAS 993-13-5).......................1C350, 1C450.b.1

methylphosphonothioic dichloride (CAS 676-98-2).......................1C350

methyl-substituted phenylene........................................8.b.1

MHN

     see methylhydrazine nitrate

micro contact printing tools......................................3B001.f.2

microbolometers..............................................6A002.a.3

microchannel plates.......................................6A002.a.2, ML15

Microcyclus ulei...............................................1C354.c.3

microcystin..................................................1C351.d.10

microfluorination ion sources.......................................3A233

microorganism cultures

     see bacterial cultures

     see biological warfare agents

     see fungi

     see virus cultures

microprocessor, microcontroller and microcomputer microcircuits

..............................................3A001.a.2, 3A001.a.3, 3E003

microwave equipment and components..................0B001.i.1, 3A001, 3A002

military vehicles

     see land vehicles and components

milling machines............................................2B001, 2B123

minelets

     see submunitions

mines (explosive) and components

     see also explosives and explosive devices

................................................................ML4

missiles, missile equipment and missile components

     see also launch and launch support equipment

     see also rockets, rocket equipment and components

................................................................ML4

     accelerometers for.........................................7A101, 7A103

     combustion regulation equipment....................................9A118

     components usable in............................................9A108

     control systems.................................................5A101

     for military use...................................................ML4

     guidance sets............................................7A117, 7D103

     navigation systems.........................................7A102, 7A103

     precision tracking systems for.......................................6A108

     propulsion systems and components...........9A101, 9A105, 9A106, 9A109, 9A111

     radar cross-section measurement systems and components................6B108

     reentry vehicles usable with........................................9A116

     software for....................................................6D103

     staging mechanisms.............................................9A117

     thermal batteries................................................3A102

     wind tunnels for.................................................9B105

mission-abort assessment systems

     see damage assessment systems

MMICs

     see monolithic integrated circuits

mobile gas liquefying equipment......................................ML4

mobile repair shops and related equipment.............................ML17

MOCVD equipment

     see chemical vapour deposition equipment

modeccin...................................................1C351.d.17

models (simulations)

     see simulators and simulator components

     see software

modular electrical pulse generators...................................3A229

molecular beam mass spectrometers

     see mass spectrometers and ion sources

molecular laser isotopic separation plant

     see isotope separation plants, systems, equipment and components

molecular pumps..............................................0B001.b.9

molybdenum and molybdenum alloys

     coating technology...............................................2E003

     in fibrous form..................................................1C010

     spherical particles of.............................................1C117

MON

     see nitrogen and nitrogen compounds

monitoring systems

     see sensors and detectors

     see surveillance systems

monkey pox virus.............................................1C351.a.12

monolithic integrated circuits...............................3A001, 3A001.b.2

monolithic mirrors.............................................6A004.a.2

monomers........................................................ML8

monomethyl hydrazine (CAS 60-34-4)........................1C111.a.4, ML8.c.4

monospectral imaging sensors......................................6A002

mortars..........................................................ML2

MOS controlled thyristors..........................................3A001

motion simulators

     see also simulators and simulator components

...............................................................2B120

motors and motor components

     see engines and engine components

moulds

     for isostatic presses..............................................2B204

     for superplastic forming and diffusion bonding...........................1B003

     for the production of composite structures..............................1B101

movable nozzle control systems

     see rocket propulsion systems

MPA

     see N-nonanoylmorpholine

MPMs

     see microwave equipment and components

MRF

     see magnetorheological finishing tools

multichip integrated circuits........................................3A001

multi-data-stream processing equipment...............................4D003

multidirectional, multidimensional weaving machines.....................1B001

multi-element detector arrays

     see sensors and detectors

multi-layer masks for integrated circuits

     see semiconductor manufacturing equipment

multilevel security capability equipment

     see information security systems

multimode optical fibre and cables, high tensile strength

     see optical fibre, equipment and accessories

multiple domed combustors, technology for development and production of 9E003.a.1

multiple-seal pumps...............................................2B350

multipoint initiation systems

     see detonation equipment

multisensor mission management systems, technology for..............7E004.b.6

multispectral imaging sensors.......................................6A002

multistage light gas guns

     see gas guns

multi-walled piping................................................2B350

Murray Valley encephalitis virus..................................1C351.a.23

mustard gas

     see chemical warfare agents and precursors

     see nitrogen and nitrogen compounds

Mycoplasma capricolum subsp. Capripneumoniae....................1C352.b.2

Mycoplasma mycoides subsp. Mycoides............................1C352.b.1

mycoplasmas....................................................1C352

>>===============================<<

>>N<<

N-(2-nitrotriazolo)-2,4-dinitroimidazole

     see NTDNIA

N,N diallylhydrazine, as propellant.................................1C111.a.4

N,N-dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-ols and corresponding protonated salts              1C450.b.5

N,N-dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-thiols and corresponding protonated salts              1C450.b.6

N,N-dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethyl-2-chlorides and corresponding protonated salts              1C450.b.4

N,N-dialkyl [methyl, ethyl or propyl (normal or iso)] phosphoramidic dihalides1C450.b.2

N,N-diisopropyl-(beta)-amino ethanol (CAS 96-80-0)......................1C350

N,N-diisopropyl-(beta)-aminoethane thiol (CAS 5842-07-9).................1C350

N,N-diisopropyl-(beta)-aminoethyl chloride (CAS 96-79-7)..................1C350

N,N-diisopropyl-(beta)-aminoethyl chloride hydrochloride (CAS 4261-68-1)....1C350

N,N-dimethyl phosphoramidic dichloride (CAS 677-43-0)..................1C350

N,N-dimethylaminophosphoryl dichloride

     see diethyl methylphosphonate

N,N-diphenylurea...................................................ML8

nanocrystalline alloy strips.........................................1C003

nano-imprint lithography tools....................................3B001.f.2

naphthalene..................................................1C008.b.1

natural uranium

     see uranium metal, uranium alloys, and uranium compounds

naval vessels

     see marine vessels, equipment and components

     see submersible vessels, equipment and components

navigation systems, equipment and components

     see also global navigation satellite systems

     see also sensors and detectors

............................................................7A, 7A105

     acoustic underwater systems....................................6A001.a.1

     avionics systems................................................7D003

     data-based reference navigation equipment...........7A003, 7D003.b.3, 7E004.a.6

     direction finding systems....................5A001, 7A115, 7D003.d.5, 7E004.a.1

     electronic......................................................ML11

     for helicopters...............................................7E004.c.2

     for missiles..............................................7A117, 7D103

     for submersible vehicles...........................................8A002

     for unmanned airborne vehicles..................................9A012.b.2

     global navigation satellite systems...................................7A003

     inertial navigation systems.................................7A003, 7E004.a.4

     integrated navigation systems.......................................7A103

     ocean salvage systems...........................................8A001

     passive coherent location systems...................................5A001

     passive direction finding systems....................................7A115

     piloting systems for parachuted loads..................................ML10

     production facilities for............................................7B103

     software for....................................................7D002

     sonar navigation systems.................................6A001.a.2, 7A008

     terrain contour mapping equipment...................................6A108

     True North determination equipment.........................7A003, 7A003.c.1

NBC detection systems

     see nuclear, biological and chemical detection systems

N-butyl-ferrocene (CAS 31904-29-7)..................................ML8.f.4

NDT

     see non-destructive test equipment

negative hydrogen ion beam current injectors...........................ML19

NENAs (CAS 85954-06-9, CAS 85068-73-1, CAS 85068-73-1, CAS 82486-83-7, CAS 82486-82-6, CAS 17096-47-8)              ML8.e.14

neodymium lasers................................................6A205

neopentyl[diallyl]oxy, tri[dioctyl]phosphato-titanate (CAS 110438-25-0, CAS 103850-22-2)ML8.f.15

neptunium-237...................................................1C012

nerve agents

     see chemical warfare agents and precursors

nets for submersible vessels and torpedoes

     see submersible vessels, equipment and components

network analysers................................................3A002

neural computers, assemblies and components.........................4A004

neural network integrated circuits.................................3A001.a.9

neutron detection and measuring instruments, for nuclear reactors..........0A001

neutron generator systems.........................................3A231

Newcastle disease virus.........................................1C352.a.9

NG

     see nitroglycerin

nickel, nickel alloys and nickel compounds..........................1C002.b.1

     chemical handling equipment made with...............................2B350

     nickel aluminides.............................................1C002.a.1

     nickel--graphite coating technology...................................2E003

     porous nickel metal..............................................1C240

     powdered.....................................................1C240

     qualified for turbine engines.....................................1C002.c.1

niobium and niobium alloys........................1C002.b.2, 1C002.c.1, 2B350

Nipah virus..................................................1C351.a.32

nitrate groups, compounds containing...............................ML8.e.6

nitratoethylnitramine compounds

     see NENAs

nitraza groups, compounds containing...............................ML8.e.6

nitric acid, liquid oxidisers containing...............................ML8.d.10

nitrided niobium-titanium-tungsten alloy............................2A225.a.2

nitro groups, compounds containing.................................ML8.e.6

nitrocellulose.....................................................ML8

nitrogen and nitrogen compounds

     see also ADN

     see also ammonia-hydrogen exchange plants (crackers)

     see also AP

     see also NTAT

     ammonia synthesis units..........................................1B227

     ammonium bifluoride.............................................1C350

     ammonium picrate................................................ML8

     mixed oxides of nitrogen........................................1C111.a.3

     nitrogen dioxide (CAS 10102-44-0)................................1C111.a.3

     nitrogen mustards..............................................ML7.b.2

     nitrogen trifluoride..............................................ML8.d.3

     nitroglycerin (CAS 55-63-0)..........................................ML8

     nitroguanidine (CAS 556-88-7)..................................1C011, ML8

     nitrostarch......................................................ML8

N-methyl-P-nitroaniline (CAS 100-15-2)...............................ML8.f.13

NNHT (CAS 130400-13-4).........................................ML8.a.31

N-nonanoylmorpholine (CAS 5299-64-9)......................1A004.a.4, ML7.d.6

noble metal modified aluminides, coating technology.....................2E003

noise reduction systems

     for marine vessels.......................................8A002, 8A002.o.3

     for underwater use...............................................8A002

     propellers and propfans...........................................8E002

non-composite ceramic materials

     see ceramic materials

non-contact type measuring systems...............................2B006.b.1

non-destructive test equipment......................................9B007

non-fluorinated polymeric substances...........................1A003, 1C008

non-linear optical materials

     see optical components and equipment

non-magnetic diesel engines, for military use..........................ML9.b.3

non-planar absorbers

     see electromagnetic equipment

non-tunable lasers

     see laser beam systems

nozzles for aerodynamic isotope separation

     see isotope separation plants, systems, equipment and components

nozzles for pyrolitic deposition

     see pyrolised materials and pyrolisis equipment

nozzles for rocket propulsion systems

     see also rocket propulsion systems

...............................................................9A008

     control systems.............................................9E003.a.10

     usable in missiles..........................................9A106, 9A108

N-pyrrolidinone....................................................ML8

NQ

     see nitroguanidine

NTAT........................................................ML8.a.25

NTDNA (CAS 75393-84-9).........................................ML8.a.32

NTDNIA......................................................ML8.a.16

NTDNT.......................................................ML8.a.32

NTNMH.......................................................ML8.a.17

NTNT........................................................ML8.a.25

NTO (CAS 932-64-9).............................................ML8.a.18

nuclear precession magnetometers................................6A006.a.2

nuclear reactors and reactor components...........................0A, 0A001

     control systems.................................................0A001

     for military use..................................................ML17

     fuels and propellants for.....................................0B005, 0B006

     metallic heat sources.............................................1C012

     pressure vessels and tubes........................................0A001

nuclear, biological and chemical detection systems......................1A004

nucleic acid sequences

     see genetic elements

numerically controlled machine tools.................................2B001

     co-ordinate measuring machines....................................2B006

     dimensional inspection machines, instruments and systems.................2B206

     for gear production...............................................2B003

     for optical finishing...............................................2B002

     software for....................................................2D002

     spin-and flow-forming machines..........................2B009, 2B109, 2B209

     technology for operating...........................................2E003

>>===============================<<

>>O<<

O,O-diethyl phosphorodithioate (CAS 298-06-6).........................1C350

O,O-diethyl phosphorothioate (CAS 2465-65-8)..........................1C350

O,O-diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (CAS 78-53-5).....1C450.a.1

O-alkyl alkyl-phosphonofluoridates..................................ML7.b.1

O-alkyl N,N-dialkyl phosphoramidocyanidates.........................ML7.b.1

O-alkyl O-2-dialkyl aminoethyl alkyl phosphonites......................ML7.c.2

O-alkyl-aminoethyl alkyl phosphonothiolates..........................ML7.b.1

object detection and location systems

     see also sensors and detectors

............................................................6A001.a.1

ocean salvage systems............................................8A001

O-Chlorobenzylidenemalononitrile

     see [(2-chlorophenyl) methylene] propanedinitrile

octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazine

     see HMX and derivatives

octahydro-2,5-bis(nitroimino)imidazo [4,5-d]imidazole

     see BNNII

octogen

     see HMX and derivatives

octogene

     see HMX and derivatives

O-ethyl s-2-diisopropylaminoethyl methyl phosphonothiolate

     see VX

O-ethyl s-phenyl ethylphosphonothiolothionate

     see fonofos

O-ethyl-2-di-isopropylaminoethyl methylphosphonite (CAS 57856-11-8)......ML7.c.2

O-ethyl-N,N-dimethylphosphoramidocyanidate

     see tabun

O-isopropyl methylphosphonochloridate (CAS 1445-76-7)................ML7.c.3

O-isopropyl methylphosphonofluoridate

     see sarin

Omsk haemorrhagic fever virus..................................1C351.a.24

on board weapon control systems

     see weapons control systems

on-line control systems

     for aerospace design and testing....................................9B005

     for gas turbine manufacture........................................9B002

ONTA

     see NTO

operating systems software

     see also software

     for multi-data-stream processing equipment............................4D003

O-pinacolyl methylphosphonochloridate..............................ML7.c.4

O-pinacolyl methylphosphonofluoridate

     see soman

optical (infrared) tracking (range) radars

     see radar systems and components

optical components and equipment

     see also optical fibre, equipment and accessories

     see also optical mirrors

     see also sensors and detectors

.........................................................6A002, 6A004

     coherent optical transmission and detection equipment..................5E001.c.2

     for measurement and testing.......................................6B004

     Kerr cells...................................................6A203.b.4

     non-linear optical materials.........................................6C004

     optical computers...............................................4A004

     optical control equipment..........................................6A004

     optical detectors and sensors.......................................6C002

     optical integrated circuits..........................................3A001

     optical switching technology and software...................5B001.b.3, 5E001.c.3

     optically pumped technology.....................................6A006.a.2

     Pockel cells.................................................6A203.b.4

     projection telescopes...........................................6A005.f.4

optical fibre, equipment and accessories...............................5A001

     gyro coil winders................................................7B003

     hull penetrators and connectors.................................8A002, ML9

     image inverters..................................................ML15

     in hydrophones..............................................6A001.a.2

     magnetometers......................................6A006.a.4, 6A006.a.5

     sensitive...................................................6A002.d.3

optical finishing machine tools......................................2B002

optical mirrors...................................................6A004

     beam steering mirrors..........................................6A004.a.4

     calibration equipment.............................................7B002

     with cooling systems..........................................6A005.e.1

optical surface coating and treatment technology

     see surface coating and processing materials and equipment

organic materials

     see also composite material components and structures

     explosives...................................................ML8.a.34

     fibrous and filamentary materials............................1C010, 1C010.e.2

     matrix materials.................................................1A002

     organo--inorganic compounds......................................3C003

     organo--metallic coupling agents...................................ML8.f.15

Oropouche virus....................................1C351.a.25, 1C351.a.26

ovens for UF6 isotope separation equipment............................0B002

overlay coatings

     see surface coating and processing materials and equipment

over-the-wall manipulators..........................................2B225

oxidisers................................................1C111.a.3, ML8

oxygen and oxygen compounds

     liquid oxygen converters...........................................ML10

     mixed oxides of nitrogen........................................1C111.a.3

     oxalyl chloride..................................................1C350

     oxide coating technology..........................................2E003

     oxygen iodine lasers...........................................6A005.d.5

>>===============================<<

>>P<<

pack cementation.................................................2E003

packed liquid--liquid exchange columns............................1B233.b.1

paints

     see surface coating and processing materials and equipment

parachutes......................................................ML10

paragliders....................................................ML10.h.3

para-hydrogen Raman shifters.......................................6A205

parametric technical databases (libraries)............................1E, ML17

particle beam systems for directed energy weapons.......................ML19

particulate metal fuels

     see fuels and propellants and related equipment

     see metals

passive coherent location systems...................................5A001

passive direction finding systems....................................7A115

passive sensors, in aircraft missile protection systems.....................ML4

pathogens

     see animal pathogens

     see human pathogens

     see plant pathogens

PBAA

     see polybutadiene-acrylic acid

PBAN

     see polybutadiene-acrylic acid-acrylonitrile

PCLs

     see passive coherent location systems

PDNT........................................................ML8.a.32

pellicular macro-reticulated resins.................................0B001.f.1

pentaboranes (CAS 19624-22-7, CAS 18433-84-6).......................ML8.c.3

pentaerythritoltetranitrate............................................ML8

pentyl ferrocene (CAS 1274-00-6)..................................1C111.c.6

perchlorates composited with high energy fuels........................ML8.c.7

perfluoroaliphatic-ethers........................................1C006.d.1

perfluoropolyalkylether-triazines..................................1C006.d.1

permanent magnet electric engines................................8A002.o.2

personal radiation monitoring dosimeters, sensors and detectors for.........1A004

personalised smart card systems....................................5A002

peste des petits ruminants virus.................................1C352.a.10

PETN

     see pentaerythritoltetranitrate

PFIB (CAS 382-21-8)............................................1C450.a.2

PG/LAs (programmable gate/logic arrays)

     see field programmable gates, logic arrays and interconnects

PGN (CAS 27814-48-8)...........................................ML8.e.15

phase conjugators.................................................ML19

phase measuring equipment

     see signal processing equipment

phased-array systems

     see also optical mirrors

     see also radar systems and components

....................................................6A004.d.4, 6A005.f.2

phenarsazine chloride

     see 10-chloro-5,10-dihydrophenarsazine

phenolic resin impregnated carbon materials...........................1C010

phenyl substituted phenylene....................................1C008.b.1

phenylacyl chloride (CAS 532-27-4)

     see 2-chloro-1-phenylethanone

phenylene and phenylene compounds.....................1C006.b.1, 1C008.b.1

phosgene (carbonyl chloride) (CAS 676-99-3)....................1C450.a.3, ML7

phosphorus and phosphorus compounds

     see also methyl-phosphonic acid

     phosphate glass................................................6C004

     phosphor bronze mesh packings....................................1A226

     phosphorus oxychloride (CAS 10025-87-3).............................1C350

     phosphorus pentachloride (CAS 10026-13-8)...........................1C350

     phosphorus trichloride (CAS 7719-12-2)...............................1C350

     subtrate materials for integrated circuits..........................3C003, 3C004

photocathodes................................................6A002.a.2

photoconductive arrays

     see focal plane arrays

photographic equipment

     see camera systems, camera equipment, and camera components

     see film processing equipment

photomultiplier tubes..............................................6A202

photovoltaic arrays

     see focal plane arrays

physical vapour deposition technology................................2E003

piezoelectric polymers and copolymers.......................1A001, 6A001.a.2

piloting systems for parachuted loads

     see also navigation systems, equipment and components

...............................................................ML10

pinacolone (CAS 75-97-8)...........................................1C350

pinacolyl alcohol (CAS 464-07-3).....................................1C350

pingers......................................................6A001.a.1

piping and header systems for UF6 isotope separation equipment...........0B002

pistols

     see also firearms and firearm components

................................................................ML1

pistons, using ceramic materials...................................9E003.f.1

pitch-impregnated fibres

     see preforms and prepegs

pivot-cup assembly bearings.....................................0B001.b.8

planar absorbers.................................................1C001

plant pathogens..................................................1C354

plasma equipment and components

     arc tunnels....................................................9B005

     CVD equipment........................................2B005.a.1, 3B001

     furnaces......................................................2B227

     isotope separation equipment....................................0B001.a.8

     metal powder generators..........................................1B102

     plasma separation process.........................................0B001

     propulsion systems...............................................ML12

     spraying equipment........................................2B005, 2E003

plasmids

     see genetic elements

plasticisers.......................................................ML8

platinized catalysts...............................................1A225

platinum coating technology........................................2E003

plug-ins for instrumentation cameras...............................6A003.a.6

plutonium and plutonium compounds and isotopes......................1C012

     conversion plant and equipment.....................................0B006

pneumatic tyre casings..............................................ML6

Pockel cells..................................................6A203.b.4

poly nitratomethylmethyloxetane

     see poly-NIMMO

poly phenylene-vinylene, intrinsically conductive polymers based on........1C001

poly(epichlorohydrin)............................................ML8.e.13

poly(epichlorohydrindiol).........................................ML8.e.13

poly(nitratomethyl oxirane)

     see PGN

poly[3-nitratomethyl-3-methyloxetane]

     see poly-NMMO

poly-2,2,3,3,4,4-hexafluoropentane-1,5-diol formal

     see FPF-1

poly-2,4,4,5,5,6,6-heptafluoro-2-tri-fluoromethyl-3-oxaheptane-1,7-diol formal

     see FPF-3

polyaniline, intrinsically conductive polymers based on...................1C001

polyarylene ketones, in thermoplastic liquid crystal copolymers............1C008

polyarylene sulphides, in thermoplastic liquid crystal copolymers...........1C008

polybenzothiazoles, technology for the production of........................1E

polybenzoxazoles, technology for the production of.........................1E

polybiphenylenethersulphone.......................................1C008

polybromotrifluoroethylene......................................1C006.c.3

polybutadiene--acrylic acid......................................1C111.b.3

polybutadiene--acrylic acid--acrylonitrile............................1C111.b.4

polycarbosilazanes.............................................1C007.e.3

polychlorotrifluoroethylene......................................1C006.c.2

polycyanodifluoroaminoethyleneoxide...............................ML8.f.16

polydiorganosilanes............................................1C007.e.1

polyetherimides...............................................1C010.d.1

polyfunctional aziridine amides....................................ML8.f.17

polyglycidylnitrate

     see PGN

poly-GLYN

     see PGN

polymeric substances..................................1C111, ML8, ML8.e.6

     coating technology...............................................2E003

     fibre conversion equipment.............................1B001.d.1, 1B101.c.1

     non-fluorinated............................................1A003, 1C008

poly-NIMMO (CAS 84051-81-0).....................................ML8.e.16

polynitrocubanes...............................................ML8.a.19

polynitroorthocarbonates........................................ML8.e.17

poly-NMMO (CAS 84051-81-0)

     see poly-NIMMO

polypyrrole, polymers based on......................................1C001

polysilazanes.................................................1C007.e.2

polytetrahydrofuran polyethylene glycol............................1C111.b.5

polythiophene, polymers based on...................................1C001

porcine enterovirus type 9......................................1C352.a.11

porcine herpes virus............................................1C352.a.6

porous macro-reticulated resins...................................0B001.f.1

porous nickel metal

     see nickel , nickel alloys and nickel compounds

positioning equipment

     see navigation systems, equipment and components

positioning tables.................................................2B121

potassium and potassium compounds................................1C350

     potassium amide catalyst pumps....................................1B230

     potassium nitrate.................................................ML8

     potassium titanyl arsenate......................................6C004.b.1

potato andean latent tymovirus...................................1C354.a.1

potato spindle tuber viroid.......................................1C354.a.2

powdered metal fuels

     see fuels and propellants and related equipment

     see metals

power amplifiers, microwave equipment............................3A001.b.8

power generating equipment, for directed energy weapons.................ML19

power supplies

     air independent power systems...............................8A002, ML9.b.4

     for induction furnaces.............................................2B226

     for isotope separation..........................................0B001.j.5

     high-power direct current....................................3A226, 3A227

power transmission systems

     see also engines and engine components

     for helicopters..................................................9E003

     for marine vessels...............................................8A002

     for tilt rotor/wing aircraft...........................................9E003

praseodymium-doped fluoride fibre amplifiers........................5E001.c.2

precision mandrels

     see mandrels

precision tracking systems

     see tracking systems

precursor materials

     see also chemical warfare agents and precursors

     see also explosives and explosive devices

     see also fuels and propellants and related equipment

     for composite materials...........................................1C007

preforms and prepegs

     see also fibrous and filamentary materials

...............................................................1C210

     made from fibrous and filamentary materials............................1C010

     production facilities.........................................1B001, 1B101

     resin impregnated fibre prepregs....................................9C110

pressure refuellers

     see also fuels and propellants and related equipment

...............................................................ML10

pressure regulation technology

     see also sensors and detectors

...................................................1E103, 2B230, 6A226

pressure suits

     see protective and decontamination clothing and equipment

pre-swirl and post-swirl systems..................................8A002.o.1

primary high energy cells and batteries

     see cells and batteries (electrical)

primer anvils......................................................ML3

probing (test) systems, semiconductor equipment

     see semiconductor manufacturing equipment

process systems

     for aerodynamic separation equipment.............................0B001.d.7

     for molecular laser isotope separation equipment......................0B001.h.5

     for nuclear fuel reprocessing........................................0B006

processors, digital

     see signal processing equipment

product and tails collector systems for isotope separation equipment0B001.g.3, 0B001.h.2, 0B001.i.5, 0B002

profilometers....................................................7B002

programmable gate and logic arrays

     see field programmable gates, logic arrays and interconnects

projectile launchers

     see launch and launch support equipment

projection telescopes...........................................6A005.f.4

propellants

     see fuels and propellants and related equipment

propellers and propfans

     for marine vessels...............................................8A002

     software for....................................................8D002

     technology for..........................................8E002, 9E003.b.2

     ventilated propeller systems.....................................8A002.o.2

propelling nozzles

     see nozzles for rocket propulsion systems

propulsion systems and components

     see engines and engine components

     see fuels and propellants and related equipment

     see propellers and propfans

     see rocket propulsion systems

propulsive substances

     see fuels and propellants and related equipment

propyl ferrocene (CAS 1273-89-8)..................................1C111.c.6

propyleneimine (2-methylaziridine) (CAS 75-55-8)......................ML8.f.18

protective and decontamination clothing and equipment

     see also breathing equipment

...............................................................1A004

     against chemical warfare agents......................................ML7

     armoured plate..................................................ML13

     ballistic protection materials and components........................ML13, ML6

     body armour..............................................1A005, ML13

     for high altitude parachutists......................................ML10.h.8

     full and half suits..............................................2B352.f.1

     helmets..................................................ML10, ML13

     hoods......................................................2B352.f.1

     masks........................................................ML10

protonated salts, as toxic agents.............................ML7.b.1, ML7.c.2

proximity focused image intensifier tubes...........................6A203.b.4

Pseudomonas campestris pv. Oryzae

     see Xanthomonas oryzae pv. Oryzae

Pseudomonas solanacearum

     see Ralstonia solanacearum

PTIA.........................................................ML8.a.16

Puccinia glumarum

     see Puccinia striiformis

Puccinia graminis..............................................1C354.c.4

Puccinia striiformis.............................................1C354.c.5

pulmonary & renal syndrome--haemorrhagic fever virus...............1C351.a.31

pulsating chemical vapour deposition production equipment

     see chemical vapour deposition equipment

pulse compression equipment.......................................6A008

pulse generators

     see also detonation equipment

.........................................................3A229, 3A230

pulse jet engines

     see aero-engines and components

pulse liquid rocket engines

     see rocket propulsion systems

pulse radar cross-section measurement systems and components

     see radar systems and components

pulsed electron accelerators........................................3A201

pulsed laser systems...................................6A005, 6A205, ML19

pulsers

     see modular electrical pulse generators

pumpjet propulsion systems........................................8A002

pumps

     ceramic materials in...........................................2B350.i.2

     ferrosilicon in................................................2B350.i.2

     for isotope separation equipment....................................0B002

     for potassium amide..............................................1B230

     for rocket propulsion systems.......................................9A006

     mercury amalgam pumps.......................................1B233.b.2

     molecular...................................................0B001.b.9

     multiple-seal pumps..............................................2B350

     optically pumped technology.....................................6A006.a.2

     pumpjet propulsion systems........................................8A002

     seal-less pumps................................................2B350

     stage pumps................................................0B004.b.4

     vacuum pumps...........................................0B002, 2B231

Puumala virus................................................1C351.a.31

PVD

     see physical vapour deposition technology

Pyricularia spp.

     see Magnaporthe grisea

pyroelectric television camera tubes...................................ML15

pyrolised materials and pyrolysis equipment

     see also carbon--carbon materials

     equipment and process controls.....................................2B117

     graphites......................................................1C107

     nozzles for....................................................1B116

     technology for the production of.....................................1E104

pyrophoric metal alkyls and aryls......................................ML8

pyrotechnics, pyrotechnic equipment and components.............ML2, ML4, ML8

PYX (CAS 38082-89-2)...........................................ML8.a.20

PZO

     see DDPO

>>===============================<<

>>Q<<

QAM

     see quadrature-amplitude-modulation equipment

QL

     see O-ethyl-2-di-isopropylaminoethyl methylphosphonite

Q-switched lasers

     see laser beam systems

quadrature-amplitude-modulation equipment................5B001.b.4, 5E001.c.4

quantum cryptography systems...................................5A002.a.9

quantum well equipment...........................................3E003

quartz pressure transducers

     see also sensors and detectors

...............................................................6A226

>>===============================<<

>>R<<

Ra-226

     see radium alloys and compounds

radar systems and components......................................6A008

     Doppler navigation equipment.................................6A008, 6A108

     electronically steerable phased array antennae.................5A001, 6D003.d.2

     for missiles....................................................6B108

     frequency agility technology................................5A001.b.3, ML11

     laser beam systems..............................................6A108

     pulsed cross-section measurement systems......................6B007, 6B008

     radiation hardened...............................................6A102

     range instrumentation radars....................................6A108.b.2

     sidelooking airborne radar.........................................6A008

     signal processing equipment in......................................6A008

     signature reduction equipment and materials............................1C101

     space-qualified............................................6A008, 6A108

     synthetic aperture radar...........................................6A008

     temperature-rated...............................................6A102

radiation hardened equipment

     computers..................................................4A001.a.2

     design technology...............................................7E102

     integrated circuits.............................................3A001.a.1

     radar systems..................................................6A102

     robot systems..................................................2B007

     shielding windows...............................................1A227

     telecommunications systems.......................................5A001

     video cameras..................................................6A203

radiation sensors

     see sensors and detectors

radio equipment and components.................................5A001.b.2

     digital cellular radio equipment...................................5E001.b.3

     digital demodulators..............................................ML11

     digital troposcatter-radio...........................................ML11

     digitally controlled receivers.....................................5A001.b.5

     for directed energy weapons........................................ML19

     quadrature-amplitude-modulation equipment.................5B001.b.4, 5E001.c.4

     radio-frequency signal analysers.....................................3A002

     radiotelephones for civil use........................................5A002

     receivers......................................................5A002

     spread spectrum equipment....................5A001.b.3, 5A002.a.5, 5E001.b.4

radio frequency ion excitation coils.................................0B001.i.2

radioactive materials

     adapted for use in war..............................................ML7

     protective clothing and equipment against...................1A004.a.2, 1A004.b.2

     sensors and detectors.........................................1A004.c.2

radiographic equipment..........................................1B001.f.1

radionuclides....................................................1C236

radiotelephones for civil use........................................5A002

radium alloys and compounds.......................................1C237

radome design and production software............................6D003.d.2

Ralstonia solanacearum.........................................1C354.b.5

Raman shift lasers

     see laser beam systems

ramjet engines

     see also aero-engines and components

...............................................................9A011

range instrumentation radars.....................................6A108.b.2

range-finding systems

     see target acquisition systems

range-gated illuminators, for submersible vehicles....................8A002.d.2

Rankine cycle engines, for underwater use...........................8A002.j.1

rapid beam slew capability equipment.................................ML19

rate tables

     see motion simulators

RDX and derivatives (CAS 121-82-4, CAS 115029-35-1)..................ML8.a.21

reaction vessels and reactors (chemical)...............................2B350

reactor fuels

     see fuels and propellants and related equipment

     see nuclear reactors and reactor components

reactors

     see nuclear reactors and reactor components

real-time control systems

     see flight control systems

rebreathing apparatus

     see breathing equipment

receivers, chemical

     see chemical storage tanks and containers

receivers, microwave

     see microwave equipment and components

receivers, radio

     see radio equipment and components

rechargeable batteries and cells

     see cells and batteries (electrical)

reciprocating engines

     see also engines and engine components

...............................................................ML10

recoilless rifles

     see also firearms and firearm components

................................................................ML2

recorders, imaging equipment........................................ML15

recording equipment..............................................3A002

     analogue instrumentation magnetic tape recorders.....................3A002.a.1

     digital data recorders..........................................3A002.a.6

     digital instrumentation magnetic tape data recorders....................3A002.a.4

     digital magnetic tape data recorders...............................3A002.a.2

     digital video magnetic tape recorders...............................3A002.a.2

recovery parachutes............................................ML10.h.5

recovery vehicles and related equipment........................ML10.h.5, ML6

reentry vehicles..................................................9A116

re-entry vehicles

     see also spacecraft

reflectance measuring equipment....................................6B004

reflectivity reducing materials and treatments

     see signature reduction equipment and materials

reflectometers...................................................7B102

reflectors

     see optical mirrors

refractory ceramics, wet-spinning equipment................1B001.d.3, 1B101.c.3

refractory metals, coating technology.................................2E003

refrigeration units

     see cooling systems

     see cryogenic equipment, accessories and components

refuellers for aircraft...............................................ML10

reinforced composite materials

     see composite material components and structures

reinforcement fibres, production facilities..............................1B001

remotely operated equipment

     see also unmanned airborne vehicles, systems and components

     see also unmanned submersible vehicles

     bomb disposal equipment..........................................1A006

     refuelling equipment..............................................2B350

     remote manipulators.............................................2B225

resaturated pyrolised materials

     see carbon-carbon materials

     see pyrolised materials and pyrolisis equipment

resin impregnated fibre prepregs

     see preforms and prepegs

resist materials

     see also semiconductor manufacturing equipment

...............................................................3C002

reticles

     see semiconductor manufacturing equipment

revolvers

     see also firearms and firearm components

................................................................ML1

ricin........................................................1C351.d.4

Rickettsia prowasecki...........................................1C351.b.3

Rickettsia quintana

     see Bartonella quintana

Rickettsia rickettsii.............................................1C351.b.4

Rickettsiae......................................................1C351

rifles

     see also firearms and firearm components

................................................................ML1

Rift Valley fever virus..........................................1C351.a.13

rinderpest virus..............................................1C352.a.12

ring laser gyros

     see gyros, gyro components and gyro equipment

rings, for rotor tube support......................................0B001.b.4

ring-shaped motor stators......................................0B001.b.10

riot control agents

     see also chemical warfare agents and precursors

     see also toxicological agents

     protective and decontamination clothing and equipment.................1A004.a.4

robot systems...................................2B007, 2B207, 8A002, ML17

Rochalimaea quintana

     see Bartonella quintana

Rocio virus..................................................1C351.a.27

rocket propulsion systems

     carbon-carbon materials in.........................................9A006

     control systems.................................................9A106

     hybrid systems............................................9A009, 9A109

     liquid-propellant................................9A005, 9A006, 9A105, 9A106

     motor cases...................................................9A108

     nozzles for................................9A008, 9A106, 9A108, 9E003.a.10

     pulsed........................................................9A010

     solid-propellant.................................................9A107

     tanks for......................................................9A120

     test benches and stands for........................................9B117

     thrust chambers.................................................9A006

rockets, rocket equipment and components

     see also flight control systems

     see also launch and launch support equipment

     see also rocket propulsion systems

     see also spacecraft

................................................................ML4

     individual stages................................................9A119

     insulation for...................................................9C108

     non-destructive test equipment......................................9B007

     pyrolised materials...............................................1C102

     separation mechanisms...........................................9A117

     sounding rockets...............................1A102, 9A104, 9D103, 9D105

     staging mechanisms.............................................9A117

roller bearings

     see bearings

rollers, for composite materials......................................1B101

rotary atomisation, alloys made by.................................1C002.c.2

rotary input type shaft absolute position encoders...............3A001, 3A001.e.4

rotary position feedback units.......................................2B008

rotary shaft seals for gaseous diffusion separators....................0B001.c.4

rotating bands.....................................................ML3

rotational accelerometers...........................................7A001

rotor assemblies for gas centrifuges.................0B001.b.2, 0B001.b.3, 2B228

rotor blades for gas turbine engines

     see gas turbine engines

rotor blades for helicopters......................................7E004.c.3

ROVs and RPVs

     see unmanned airborne vehicles, systems and components

ruggedised equipment

     computers and components........................................4A101

     telecommunications systems.......................................5A001

Russian Spring--Summer encephalitis virus

     see Tick-borne encephalitis virus

>>===============================<<

>>S<<

S20 and S25 photocathodes

     see photocathodes

safety cabinets for biological agents................................2B352.f.2

safety equipment

     see protective and decontamination clothing and equipment

salicylates...............................................ML8.f.1, ML8.f.9

Salmonella typhi..............................................1C351.c.10

salvage systems

     see ocean salvage systems

sarin..........................................................ML7.b.1

satellite technology

     see also spacecraft

............................................................5E001.b.1

saxitoxin.....................................................1C351.d.5

scanning cameras and systems

     see also camera systems, camera equipment, and camera components

............................................................6A003.b.2

scatterometers...................................................7B002

scene mapping and correlation equipment.............................6A108

scoops for gas centrifuges......................................0B001.b.12

scramjet engines

     see also aero-engines and components

...............................................................9A011

screw extruders...................................................ML18

SCRs

     see silicon controlled rectifiers

seal-less pumps..................................................2B350

seals

     for surface effect vessels..........................................8A002

     made from fluoroelastomers........................................1A001

secondary batteries and cells

     see cells and batteries (electrical)

security equipment

     see information security systems

segmented mirrors for space assembly

     see optical mirrors

self-contained diving apparatus.................................8A002, ML17

self-propelled guns and related equipment

     see land vehicles and components

semi-automatic smooth-bore weapons..................................ML1

semi-closed diving apparatus

     see underwater operations equipment

semiconductor lasers..................................6A005.d.1, 6A005.d.2

semiconductor manufacturing equipment

     see also integrated circuits

.........................................................3B001, 3B002

sensors and detectors

     see also image processing and enhancement equipment

     see also radar systems and components

     fabrication technology..........................................6E003.a.1

     for chemical warfare agents..........................................ML7

     for security-related equipment and systems.............................5B002

     hydrophones........................................6A001.a.2, 6D003.a.2

     imaging sensors...........................................6A002, 6A108

     linear position feedback units.......................................2B008

     nuclear, biological and chemical detection systems...................1A004, ML7

     object detection and location systems..............................6A001.a.1

     optical sensors and detectors.......................................6C002

     sensor window materials..........................................2E003

     solid state detectors...........................................6A002.c.3

Seoul virus..................................................1C351.a.31

separation mechanisms for rockets

     see rockets, rocket equipment and components

separation nozzles and tubes

     see isotope separation plants, systems, equipment and components

separator module housings, for plasma separation equipment............0B001.i.6

separators for isotopes

     see isotope separation plants, systems, equipment and components

separators, biological

     see centrifugal separators and decanters

servo valves...............................................7A116, 9A106

sesquimustard

     see chemical warfare agents and precursors

S-FIL

     see step and flash imprint lithography tools

shaker units...............................................2B116, 9B106

sheep pox virus..............................................1C352.a.13

shielding systems

     see also protective and decontamination clothing and equipment

     see also radiation hardened equipment

     see also signature reduction equipment and materials

     see also temperature-rated equipment

     design technology...............................................7E102

     shielding windows...............................................1A227

Shiga toxin...................................................1C351.d.6

Shiga-like ribosome inactivating proteins...........................1C351.d.9

Shigella dysenteriae...........................................1C351.c.11

ship positioning systems

     see navigation systems, equipment and components

shock tubes and tunnels...........................................9B005

shotguns

     see firearms and firearm components

SHPL

     see super high-powered laser system components

shrink fit machines................................................2B228

Si--

     see silicon and silicon compounds

sidelooking airborne radar..........................................6A008

sights and sighting equipment..........................ML1, ML2, ML5, ML904

signal processing equipment........................................4A003

     array processors................................................4A003

     digital technology................................................3E002

     for towed hydrophones.........................................6A001.a.2

     frequency signal generators........................................3A002

     in radar systems and components....................................6A008

     in radio devices..............................................5A001.b.6

     signal analysers.................................................3A002

     underwater cable systems......................................6A001.a.2

     wavefront measuring equipment...................................6A005.f.1

signature reduction equipment and materials.......................1C101, ML2

     for military use..................................................ML17

     for underwater use............................................8A002.d.2

     software for....................................................1D101

silencers.........................................................ML1

silent bearings

     see bearings

silicon and silicon compounds

     see also glass and glass-based materials

     see also silicon carbides

     fibres made from.............................................1C007.c.1

     fluorinated silicone fluids........................................1C006.b.2

     fused silica in optical materials......................................6C004

     Si-Al-O-N...................................................1C007.c.1

     silicide coating technology.........................................2E003

     silicon controlled rectifiers.........................................3A001

     silicon nitrides technology..........................................1E.c.4

     silicon oxide technology...........................................1E.c.1

     silicon-on-sapphire integrated circuits.................................3A001

     substrate materials for integrated circuits.............3C001, 3C005, 3C006, 3E003

silicon carbides...............................................1C007.c.1

     ceramic materials reinforced with....................................1C107

     coating technology...............................................2E003

     heat exchangers and condensers made with.........................2B350.d.9

     substrate materials for integrated circuits.........................3C001, 6C004

     technology for the production of.....................................1E.c.3

silicon intensifier target videcon tubes..............................6A203.b.4

silicon microcircuits

     see microprocessor, microcontroller and microcomputer microcircuits

silver gallium selenide..........................................6C004.b.2

silylated resists..................................................3C002

simple programmable logic equipment

     see field programmable gates, logic arrays and interconnects

simulants.......................................................1A004

simulators and simulator components

     environmental chambers..........................................9B106

     for flow environments.............................................9B005

     for gas turbine design and modelling..................................9D004

     for integrated circuit manufacture....................................3D001

     for military use..................................................ML14

     for nuclear reactors...............................................ML17

     motion simulators...............................................2B120

     of space launch and flight..........................................4A102

     software for..................................................ML21.b.2

simultaneous initiation arrangements and systems

     see detonation equipment

Sin Nombre virus.............................................1C351.a.31

single crystal casting equipment...............................9B001, 9D004

single mode optical fibre and cable

     see optical fibre, equipment and accessories

single point diamond cutting tool inserts

     see machine tool equipment, components and assemblies

single-convolution bellows.........................................2B228

SIT vidicon tubes

     see silicon intensifier target videcon tubes

skimming acoustic wave equipment................................3A001.c.1

skirts for surface effect vessels......................................8A002

slapper detonators.............................................1A007.b.3

slurry deposition equipment........................................2E003

slurry propellant control systems....................................9A106

slush hydrogen storage and transfer systems...........................9A006

small arms

     see firearms and firearm components

small waterplane area vessels.......................................8A001

smart card systems...............................................5A002

smoke projectors and generators..................................ML2, ML4

smooth-bore weapons

     see also firearms and firearm components

......................................................ML1, ML2, ML901

sodium and sodium compounds.....................................1C350

sodium lasers

     see laser beam systems

software...........................0D, 1D, 2D001, 2D101, 2D201, 2D202, ML21

     aerospace design and testing software...................................9D

     air navigation software............................................7D003

     air traffic control software.......................................6D003.d.1

     C3I software.................................................ML21.b.4

     clearance control software.........................................9D004

     composite material manufacturing software.............................1D002

     design software..................................6D003.d.2, 7D003, 8D002

     expert systems software............................2E003, 7D003, 7E004.b.6

     filament winding equipment software............................1B001, 1B201

     flight control software..........................................7D003.d.1

     flow modelling software...........................................9D004

     for computer development and use...................................4D001

     for determining biochemical effects.................................ML21.b.3

     for electromagnetic equipment......................................2D002

     for electronics development........................................4D001

     for fault tolerant equipment................................7D003.d.4, 9D003

     for marine vessels...............................................8D001

     gas turbine design software........................................9D004

     gravity gradiometer software............................6A007, 6A107, 6D003

     integrated circuit manufacturing software...................3D001, 3D004, 3D101

     Kalman filtering software..........................................7D102

     machine tool software............................................2D002

     military software..............................................ML21.b.1

     missile software.................................................6D103

     navigation software.............................7D, 7D002, 7D003.b.2, 7D102

     operating system software.........................................4D003

     optical switching software..............................5B001.b.3, 5E001.c.3

     security-related.................................................5D002

     sensor and detector software..........................................6D

     signature reduction software........................................1D101

     simulator software.............................................ML21.b.2

     sounding rocket software....................................9D103, 9D105

     space launch software......................................9D103, 9D105

     space-qualified equipment software..................................7D103

     technological development software..................................3E101

     technology for the development of.............1E102, 1E203, 2E003, 3E101, 3E102

     towed hydrophone software.......................6D003, 6D003.a.1, 6D003.a.2

     unmanned airborne vehicle software..................................9D004

     vapour deposition systems software...............................2B005.c.2

     weapons systems software......................................ML21.b.1

solar cells and arrays...........................................3A001.e.4

solenoids..............................................3A001.e.3, 3A201

solid propellant rocket engines

     see rocket propulsion systems

solid roller bearings

     see bearings

solid state amplifiers

     see microwave equipment and components

solid state cameras

     see camera systems, camera equipment, and camera components

solid state detectors............................................6A002.c.3

solid state imaging equipment

     see image processing and enhancement equipment

solid state joining equipment, tools, dies and fixtures

     see machine tool equipment, components and assemblies

solid state lasers

     see laser beam systems

solid state switching equipment

     see switching equipment

solidification systems for UF6 isotope separation equipment...............0B002

solidtrons.......................................................3A001

soman........................................................ML7.b.1

sonar navigation systems..................................6A001.a.2, 7A008

sonar signal processing equipment

     see signal processing equipment

SORGUYL

     see TNGU

sounding rockets

     see also rockets, rocket equipment and components

...............................................................9A104

     pyrolised components............................................1A102

     software for..............................................9D103, 9D105

source code

     see software

South American haemorrhagic fever..............................1C351.a.30

space launch equipment

     see launch and launch support equipment

spacecraft

     see also launch and launch support equipment

     see also rockets, rocket equipment and components

     see also space-qualified equipment

...............................................................9A004

     computer systems for.............................................4A101

     pyrolised components.......................................1A102, 1C102

     radar systems and components.....................................6A108

     reentry vehicles.................................................9A116

     solar cells and arrays for........................................3A001.e.4

     vacuum tube components.......................................3A001.b.1

space-qualified equipment..........................................9A010

     altimeters.....................................................7A106

     cryocoolers.................................................6A002.d.1

     flight control systems.............................................7A116

     focal plane arrays...............................................6A002

     global navigation satellite systems...................................7A105

     imaging sensors..............................................6A002.b.2

     negative hydrogen ion beams.......................................ML19

     optical control equipment.......................................6A004.d.2

     optical system components................................6A002.a.1, 6A004

     radar systems and components.....................................6A008

     software for....................................................7D103

spectrum analysers

     see signal processing equipment

spectrum frequency stabilisers...................................0B001.h.6

spherical aluminium powder

     see aluminium, aluminium compounds and aluminium alloys

spindle assemblies

     see machine tool equipment, components and assemblies

spin-forming machines.................................2B009, 2B109, 2B209

splat quenching, alloys made by..........................1C002.c.2, 1C002.d.3

spray booms....................................................9A350

spray cooling thermal management systems............................3A003

spraying systems for aircraft........................................9A350

spread spectrum equipment.....................5A001.b.3, 5A002.a.5, 5E001.b.4

sprytron vacuum tubes............................................3A228

sputter deposition equipment..................................2B005, 2E003

SQUID technology.............................................6A006.a.1

SR 12

     see ADN

SRAMS

     see static random-access memories

St Louis encephalitis virus......................................1C351.a.28

stabilisers (chemical)

     see explosives and explosive devices

stabilisers for marine vessels.......................................8A002

stage pumps for conversion towers................................0B004.b.4

staging mechanisms for rockets

     see rockets, rocket equipment and components

Staphylococcus aureus toxins....................................1C351.d.7

start gyros and gyro components

     see gyros, gyro components and gyro equipment

static random-access memories

     see also computers, computer assemblies and computer components

............................................................3A001.a.2

stators, ring shaped

     see engines and engine components

stealth technology

     see damping equipment (electromagnetic)

     see surface coating and processing materials and equipment

steam sterilisable freeze drying equipment.............................2B352

steels

     coating technology...............................................2E003

     maraging steels...........................................1C116, 1C216

     titanium-stabilised duplex stainless steel...............................1C118

step and flash imprint lithography tools.............................3B001.f.2

still cameras

     see camera systems, camera equipment, and camera components

Stirling cycle engines

     see also engines and engine components

.............................................................8A002.j.4

storage integrated circuits.......................................3A001.a.4

storage tanks for chemicals

     see chemical storage tanks and containers

strap down/gimbal gyros and gyro components

     see gyros, gyro components and gyro equipment

streak cameras

     see also camera systems, camera equipment, and camera components

...........................................6A003.a.3, 6A203.a.2, 6A203.b.2

stroboscopic light systems, for underwater use.......................8A002.g.1

styphnic acid

     see 2,4,6-trinitroresorcinol

subcavitating hydrofoils

     see hydrofoil vessels

submarine nets

     see also underwater operations equipment

................................................................ML9

submarines

     see submersible vessels, equipment and components

submersible vessels, equipment and components

     see also marine vessels, equipment and components

     see also propellers and propfans

     see also underwater operations equipment

.........................................................8A001, 8A002

     pressure vessels.............................................8A002.a.1

     propulsion systems and components for.................................ML9

     umbilical cables..............................................8A002.a.3

     unmanned.....................................................8A001

submunitions.....................................................ML3

substrate materials for integrated circuits.......3C001, 3C002, 3C005, 3C006, 3E003

sulphur compounds (CAS 10545-99-0, CAS 10545-99-0)

     sulphur dichloride...............................................1C350

     sulphur monochloride.............................................1C350

     sulphur mustards...............................................ML7.b.2

super high-powered laser system components....................6A005, 6E003

superalloys.....................................................2E003

supercavitating hydrofoils

     see hydrofoil vessels and components

supercavitating propellers

     see also propellers and propfans

............................................................8A002.o.1

superconductive materials and equipment..............................ML20

     in electromagnets and solenoids..................................3A001.e.3

     in electronic components..........................................3A001

     propulsion engines............................................8A002.o.2

     solenoidal electromagnets.........................................3A201

     SQUID technology............................................6A006.a.1

     superconductive composite conductors................................1C005

     technology for the production of.....................................3E003

superfine iron oxide.............................................ML8.f.19

superlattice equipment technology...................................3E003

superplastic forming technology...............................1B003, 2E003

supersonic expansion nozzles....................................0B001.h.1

super-ventilated propellers

     see propellers and propfans

surface acoustic wave equipment

     see acoustic systems, equipment and components

surface coating and processing materials and equipment

     see also signature reduction equipment and materials

.........................................................1B101, 2B005

     coatings for signature reduction.....................................1C101

     for composite materials...........................................1B101

     for inorganic overlays.............................................2B005

     McrAlX coating technology.........................................2E003

     optical surface coating and treatment technology......................6E003.a.1

surface irregularity measuring equipment..............................2B006

surface vessels and components

     see marine vessels, equipment and components

surface-effect vehicles

     see also marine vessels, equipment and components

.........................................................8A001, 8A002

surveillance systems

     see information security systems

     see sensors and detectors

     see telecommunications systems, equipment, components and accessories

sweeping equipment

     see explosives and explosive devices

     see sensors and detectors

swimming apparatus

     see breathing equipment

     see underwater operations equipment

swine fever virus..............................................1C352.a.7

swine vesicular disease virus

     see Porcine enterovirus type 9

switching equipment...................................3A001, 3A228, 5B001

symmetric algorithm encryption equipment..........................5A002.a.1

symmetrical dimethyl hydrazine (CAS 540-73-8)........................ML8.c.4

syntactic foam, for underwater use...................................8C001

synthetic crystalline laser host material................................6C005

synthetic silahydrocarbon oils....................................1C006.a.1

systolic array computers...........................................4A004

>>===============================<<

>>T<<

T-2 toxin....................................................1C351.d.15

T4

     see RDX and derivatives

tabun (CAS 77-81-6)..............................................ML7.b.1

TACOT (CAS 25243-36-1).........................................ML8.a.32

TAGN (CAS 4000-16-2)...........................................ML8.a.22

TAIW.........................................................ML8.g.4

tangential inlet flow-driven cylindrical and conical tubes

     see vortex tubes

tank destroyers

     see land vehicles and components

tank transporters

     see land vehicles and components

tanks (vehicles) and related equipment/components

     see also land vehicles and components

................................................................ML6

tanks for chemical storage

     see chemical storage tanks and containers

tantalum and tantalum compounds

     chemical handling equipment made with...............................2B350

     crucibles coated with.............................................2A225

tape-laying machines..............................................1B001

target acquisition systems.................................ML12, ML19, ML5

target damage assessment

     see damage assessment systems

TAT (CAS 41378-98-7)............................................ML8.g.5

TATB (CAS 3058-38-6)...........................................ML8.a.23

TCSEC capability

     see trusted computer system evaluation criteria capability

...................................................................0

TEA

     see triethylaluminium

tear gases and related equipment and materials

     see chemical warfare agents and precursors

     see riot control agents

technical military databases libraries, parametric

     see parametric technical databases (libraries)

technology.............................................1E, 2E001, 2E002

     for aerospace design and testing.......................................9E

     for computer development and use...................................4E001

     for development, production and use of controlled items.................0E, ML22

     for flight control..............................................7E004.b.5

     for integrated circuit manufacture..............................3E001, 3E002

     for marine vessels..................................................8E

     for metal-working processes........................................2E003

     for navigation systems, equipment and components.................7E001, 7E101

     for numerical control units.........................................2E003

     for pressure regulation............................................1E103

     for security-related equipment and systems.............................5E002

     for sensors and detectors.............................................6E

     for software development and use...................................3E101

     for telecommunications systems.....................................5E001

TEDDZ.......................................................ML8.a.24

TEGDN

     see triethylene glycol dinitrate

telecommunications systems, equipment, components and accessories

     see also radio equipment and components

...............................................................5A001

telemetering and telecontrol equipment

     see also sensors and detectors

...............................................................5A101

television systems and equipment

     see also video cameras

......................................................5A002, 8A002.d.1

tellurium, in optical sensors.........................................6C002

temperature-rated equipment

     computer systems............................................4A001.a.1

     radar systems..................................................6A102

     robot systems...................................................ML17

     telecommunications systems....................................5A001.a.3

TEMPEST type equipment

     see information security systems

     see surveillance systems

tension stretchers for composite materials

     see also optical fibre, equipment and accessories

...............................................................1B101

TEPAN (CAS 68412-45-3).........................................ML8.f.20

TEPANOL (CAS 68412-46-4).......................................ML8.f.21

TE-PVD

     see thermal-evaporation physical vapour deposition technology

terephthalic acid...............................................1C008.b.2

terrain contour mapping equipment...................................6A108

tertiary-butyl substituted phenylene................................1C008.b.1

teschen disease virus..........................................1C352.a.14

test tape for recording equipment....................................3A002

test, inspection and production equipment

     for aerospace and propulsion systems...................................9B

     for composite materials...........................................1B001

     for controlled products.............................................ML18

     for directed energy weapons........................................ML19

     for marine vessels and equipment......................................8B

     for materials processing..............................................2B

     for navigation and avionics systems.....................................7B

     for security-related equipment and systems.............................5B002

     for semiconductor production.......................................3B002

     for sensors and lasers...............................................6B

     for telecommunications and security systems.............................5B1

     test benches and stands..........................................9B117

tetraacetyldibenzylhexaazaisowurtzitane

     see TAIW

tetraethylenepentaamineacrylonitrile

     see TEPAN

tetraethylenepentaamineacrylonitrileglycidol

     see TEPANOL

tetramethylhydrazine...........................................1C111.a.4

tetranitrobenzotriazolobenzotriazole

     see TACOT

tetranitroglycoluril

     see TNGU

tetranitronaphthalene...............................................ML8

tetranitrosemiglycouril

     see K-55

tetrazoles.....................................................ML8.a.25

tetrodotoxin..................................................1C351.d.8

tetryl (CAS 479-45-8)............................................ML8.a.26

thallium arsenic selenide........................................6C004.b.3

thermal batteries.................................................3A102

thermal evaporation physical vapour deposition technology................2E003

thermal imaging equipment

     see infrared imaging equipment

thermal ionization mass spectrometers................................3A233

thermal sensors

     see infrared sensors and detectors

thermal-rated equipment

     see temperature-rated equipment

thermoplastic liquid crystal copolymers...............................1C008

thermoset resin impregnated continuous materials.......................1C210

thickeners

     see fuels and propellants and related equipment

thiodiglycol (CAS 111-48-8).........................................1C350

thionyl chloride (CAS 7719-09-7).....................................1C350

thiophosphoryl chloride (CAS 3982-91-0)...............................1C350

three axis magnetic heading sensors..................................7A103

through-the-wall manipulators.......................................2B225

thrust chambers for rocket propulsion systems.........................9A006

thrust vector control sub-systems..............................9A106, 9A108

thulium--YAG lasers...............................................6A005

thulium--YSGG lasers..............................................6A005

thyristors.......................................................3A001

tick-borne encephalitis virus....................................1C351.a.14

tilt rotor and tilt wing aircraft

     see also aircraft and aircraft components

...............................................................9E003

tilting spindles...................................................2B008

TIMS

     see thermal ionization mass spectrometers

tip shroud castings..............................9B001, 9E003.a.4, 9E003.a.5

titanium, titanium alloys and titanium compounds......1C002.b.3, 1C002.c.1, 1C202

     borides of titanium.............................1C007, 1C007, 1C007, 1C007

     chemical handling equipment made with...............................2B350

     coating technology for............................................2E003

     diffusion bonding technology for..................................2E003.b.2

     superplastic technology...................................1B003, 2E003.b.2

     titanium aluminides...........................................1C002.a.2

     titanium subhydride.............................................ML8.c.9

     titanium tetrachloride (titanium IV) compounds.........................ML8.f.15

     titanium-doped sapphire...........................................6C005

     titanium--sapphire lasers..........................................6A005

     titanium-stabilised duplex stainless steel...............................1C118

     with uranium...................................................1C004

TMA

     see trimethylaluminium

TMETN

     see trimethylolethane trinitrate

TMP

     see trimethyl phosphite

TNAD (CAS 135877-16-6).........................................ML8.a.27

TNAZ (CAS 97645-24-4)..........................................ML8.a.28

TNGU (CAS 55510-03-7)..........................................ML8.a.29

TNP (CAS 229176-04-9)..........................................ML8.a.30

TNT

     see 2,4,6-trinitrotoluene

tools

     see machine tool equipment, components and assemblies

torpedoes, components and equipment

     see also explosives and explosive devices

     see also underwater operations equipment

................................................................ML4

     torpedo nets.....................................................ML9

towed acoustic hydrophone arrays

     see hydrophones

tow-placement machines...........................................1B001

toxicological agents

     see also biological warfare agents

     see also chemical warfare agents and precursors

     see also protective and decontamination clothing and equipment

.....................................................1C351, 1C450, ML7

     monitoring systems for............................................2B351

     precursor materials..............................................1C350

     riot control agents.................................................ML7

TPB (CAS 603-33-8)..............................................ML8.f.22

TPEG

     see polytetrahydrofuran polyethylene glycol

tracking systems

     see also navigation systems, equipment and components

     see also radar systems and components

     automatic.....................................................6A008

     for directed energy weapons........................................ML19

     for kinetic energy weapons.........................................ML12

     for missiles....................................................6A108

trailers

     see also land vehicles and components

................................................................ML6

training equipment................................................ML14

trajectory technology

     see rocket propulsion systems

transceivers

     see radio equipment and components

transducers

     see also sensors and detectors

......................................................6A001.a.1, 9B008

transfer lasers................................................6A005.d.5

transient recorders

     see waveform digitisers

transistors for microwave equipment...............................3A001.b.3

transmitters

     see radio equipment and components

transposons

     see genetic elements

travelling wave tubes...........................................3A001.b.1

tray exchange towers

     see isotope separation plants, systems, equipment and components

triaminoguanidinenitrate

     see TAGN

triaminotrinitrobenzene

     see TATB

triazines......................................................ML8.a.31

triazoles......................................................ML8.a.32

trichloronitromethane...........................................1C450.a.7

triethanolamine (CAS 102-71-6)......................................1C350

triethanolamine hydrochloride (CAS 637-39-8)...........................1C350

triethyl phosphite (CAS 122-52-1).....................................1C350

triethylaluminium..................................................ML8

triethylene glycol dinitrate (CAS 111-22-8).......................1C111.c.2, ML8

triggered spark-gaps..............................................3A228

triisopropyl phosphite (CAS 116-17-6).................................1C350

trimethyl phosphite (CAS 121-45-9)...................................1C350

trimethylaluminium.................................................ML8

trimethylhydrazine.............................................1C111.a.4

trimethylolethane trinitrate.......................................1C111.c.4

trinitroanisol......................................................ML8

trinitroglycerine....................................................ML8

trinitronaphthalene.................................................ML8

trinitrophenylmethylnitramine

     see tetryl

trinitroxylene......................................................ML8

triol.........................................................ML8.e.13

triphenyl bismuth

     see TPB

tris (2-chloroethyl) amine (CAS 555-77-1).......................ML7.b.2, ML7.c.3

tris vinoxy propane adduct

     see TVOPA

tris-1-(2-methyl)aziridinyl phosphine oxide

     see MAPO and derivatives

tritium....................................................1B231, 1C235

True North determination equipment..........................7A003, 7A003.c.1

trusted computer system evaluation criteria capability

     see computers, computer assemblies and computer components

tumblers........................................................ML18

tunable band-pass filters........................................3A001.b.5

tunable lasers

     see also laser beam systems

.........................................................6A005, 6A205

tungsten, tungsten alloys and tungsten compounds

     coating technology...............................................2E003

     spherical particles of.............................................1C117

     tungsten carbide................................................1C226

     with uranium...................................................1C004

turbine engines

     see gas turbine engines

turbocharger systems technology..................................9E003.f.2

turboexpanders and turboexpander compressors........................1B232

turbofan, turbojet and turboprop engines

     see also aero-engines and components

.........................................................9A101, 9A102

turning machines.................................................2B001

TV cameras

     see video cameras

TVOPA (CAS 53159-39-0).........................................ML8.e.18

two dimensional focal plane arrays

     see focal plane arrays

tyres, bullet-proof..................................................ML6

>>===============================<<

>>U<<

UAVs

     see unmanned airborne vehicles, systems and components

UF6

     see uranium metal, uranium alloys, and uranium compounds

ultrasonic testing machines, for defect inspection.....................1B001.f.2

ultra-wideband modulation equipment..............................5A001.b.4

umbilical cables for submersible vessels............................8A002.a.3

UN class 1.1 solid propellants......................................ML8.b.1

UN class 1.3 solid propellants......................................ML8.b.2

underwater operations equipment

     see also acoustic systems, equipment and components

     see also submersible vessels, equipment and components

.............................................................8A002.j.1

     acoustic location systems.......................................6A001.a.1

     air independent power systems...............................8A002, ML9.b.4

     bathymetric survey systems.....................................6A001.a.1

     countermeasure equipment.........................................ML11

     detection equipment...............................................ML9

     electric field sensors.............................................6A006

     laser beam systems...........................................5A001.b.1

     navigation systems......................................6A001.a.1, 7A008

     optical fibre equipment.........................................5A001.c.2

     self-contained diving apparatus................................8A002, ML17

     signal processing equipment.....................................6A001.a.2

     syntactic foam..................................................8C001

     untethered communications systems...............................5A001.b.1

underwater vessels

     see submersible vessels, equipment and components

unmanned airborne vehicles, systems and components

     see also aircraft and aircraft components

..........................................................9A012, ML10

     autonomous programmable......................................ML10.c.1

     combustion regulation equipment....................................9A118

     flight control systems..................................7E004.b.4, 7E004.b.5

     production facilities..............................................9B010

     pulse jet engines for..............................................9A111

     remotely piloted air vehicles......................................ML10.c.1

     software for....................................................9D004

     turboprop engines for.............................................9A102

unmanned launchers

     see launch and launch support equipment

unmanned submersible vehicles.....................................8A001

unprocessed fluorinated compounds.................................1C009

unsymmetrical dimethyl hydrazine (CAS 57-14-7).......................ML8.c.4

unsymmetrical dimethylhydrazine nitrate............................1C111.a.4

unsymmetrical diphenylurea

     see N,N-diphenylurea

uranium metal, uranium alloys, and uranium compounds..................1C004

     conversion plant and equipment.....................................0B003

     isotope separation equipment.......................................0B001

>>===============================<<

>>V<<

vacuum atomisation, alloys made by...............................1C002.c.2

vacuum furnaces

     see furnaces

vacuum headers..................................................0B002

vacuum housings..............................................0B001.j.3

vacuum manifolds................................................0B002

vacuum microelectronic equipment

     see microprocessor, microcontroller and microcomputer microcircuits

vacuum pumps.............................................0B002, 2B231

vacuum tubes and valves (electronic)...................3A001.b.1, 3A228, 3E003

valves (electronic)

     see vacuum tubes and valves (electronic)

valves (mechanical)...............................................2A226

     bellows seal valves....................0B001.b.13, 0B001.c.6, 0B001.d.6, 2A226

     containing aluminium.............................................2A226

     for handling chemicals............................................2B350

     servo valves..............................................7A116, 9A106

     with fluoroelastomers.............................................1A001

vanes for gas turbine engines

     see also gas turbine engines

..............................................9B001, 9E003.a.4, 9E003.a.5

vapour deposition equipment.....................................1B101.c.2

Variola virus.................................................1C351.a.15

vector processors and assemblies..............................3E002, 4A003

vectors (genetic)

     see genetic elements

vehicles

     see aircraft and aircraft components

     see land vehicles and components

     see marine vessels, equipment and components

     see spacecraft

     see submersible vessels, equipment and components

velocity interferometers............................................6A225

Venezuelan equine encephalitis virus..............................1C351.a.16

ventilated full and half (protective clothing) suits

     see protective and decontamination clothing and equipment

ventilated propellers

     see propellers and propfans

verotoxin producing strains.........................................1C353

verotoxin ribosome inactivating proteins............................1C351.d.9

vesicant agents.................................................ML7.b.2

vesicular stomatitis virus.......................................1C352.a.15

vessels of war

     see marine vessels, equipment and components

     see submersible vessels, equipment and components

vibration test systems, equipment and components................2B116, 9B006

Vibrio cholerae...............................................1C351.c.12

videcon tubes.................................................6A203.b.4

video cameras

     see also camera systems, camera equipment, and camera components

...............................................................6A203

     for underwater use............................................8A002.d.1

     with solid state sensors.........................................6A003.b.1

vinylidene fluoride materials..................................1A001, 1C009

virus cultures

     see also animal pathogens

     see also human pathogens

     see also plant pathogens

........................................................1C351, ML7.i.2

VISARS

     see velocity interferometers

viscum album lectin 1..........................................1C351.d.19

vision systems

     see image processing and enhancement equipment

volkensin...................................................1C351.d.18

vortex tubes

     see isotope separation plants, systems, equipment and components

VX...........................................................ML7.b.1

>>===============================<<

>>W<<

wafers and wafer handling equipment

     see semiconductor manufacturing equipment

warships

     see marine vessels, equipment and components

water jet cutting machines

     see machine tool equipment, components and assemblies

water tunnels....................................................8B001

water-hydrogen sulphide exchange plants.............0B004.a.1, 0B004.b.1, 1B229

water-screw propeller systems

     see propellers and propfans

waveform digitisers............................................3A002.a.5

wavelength division multiplexing technology

     see coherent optical transmission and detection equipment

wax pattern preparation equipment

     see ceramic materials

weapon sights

     see sights and sighting equipment

weapons

     see ammunition and components

     see firearms and firearm components

     see missiles

     see smooth-bore weapons

...................................................................0

weapons control systems....................................ML21.b.1, ML5

weaving machines, multidimensional.................................1B001

western equine encephalitis virus................................1C351.a.17

wet-spinning equipment

     see ceramic materials

white pox...................................................1C351.a.18

wide-swath bathymetric survey systems

     see bathymetric survey systems

wind tunnels......................................9B005, 9B105, 9E003.b.1

windows for nuclear radiation shielding

     see radiation hardened equipment

work stations

     see computers, computer assemblies and computer components

>>===============================<<

>>X<<

Xanthomonas spp..............................................1C354.b.1

xenon flash-lamp drivers...........................................3A229

X-ray equipment

     see radiographic equipment

xylyl bromide......................................................ML7

>>===============================<<

>>Y<<

yellow fever virus.............................................1C351.a.19

Yersinia pestis...............................................1C351.c.13

yttrium oxide, crucibles coated with................................2A225.a.2

>>===============================<<

>>Z<<

zinc and zinc compounds

     zinc selenide.............................................6A004, 6C004

     zinc sulphide.............................................6A004, 6C004

zirconium and zirconium compounds.................................1C234

     as propellants...............................................1C111.a.2

     chemical handling equipment made with...............................2B350

     in particle form.................................................1C011

     in powder fuel.................................................ML8.c.5

     zirconium dioxide (zirconia)........................................2E003

     zirconium fluoride...............................................6C004

     zirconium oxides........................................1E.c.1, 2A225.a.2

     zirconium tubes for nuclear reactors..................................0A001

zoonoses

     see also animal pathogens

...............................................................1C351

>>===============================<<

 


[1]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established.

[2]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[3]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[4]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[5]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[6]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[1] 

[7] Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[8]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[9]  Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established

[*]  The numbers in parenthesis refer to the Notes following this Table.