Defence and Strategic Goods List 2019 (Cth)

Defence and Strategic Goods List 2019

I, Christopher Pyne, Minister for Defence, make the following instrument.

Dated 21 March 2019

Christopher Pyne

Minister for Defence

Contents

Part 1A—Preliminary 1

Division 1—Preliminary 1

1............ Name............................................................................................................................. 1

1A......... Commencement............................................................................................................. 1

2............ Authority....................................................................................................................... 1

2A......... Schedules...................................................................................................................... 1

Division 2—Simplified outline of the Defence and Strategic Goods List 2

Division 3—Interpretation 3

3.1Definitions..................................................................................................................... 3

3.2Notes............................................................................................................................. 3

3.3Incorporated goods........................................................................................................ 3

3.4New and used goods..................................................................................................... 3

3.5CAS numbers................................................................................................................ 3

3.6Source code................................................................................................................... 3

3.7Medical equipment........................................................................................................ 4

3.8Nuclear technology note (NTN).................................................................................... 4

3.9General technology note (GTN).................................................................................... 4

3.10General software note (GSN)........................................................................................ 4

3.11General “information security” note (GISN)................................................................. 5

Division 4—Definitions 6

Division 5—Acronyms and abbreviations 26

Part 1—Munitions list 30

Part 2—Dual‑use list 62

Category 0—Nuclear materials, facilities and equipment 62

Category 1—Materials, chemicals, microorganisms and toxins 75

Category 2—Materials processing 124

Category 3—Electronics 162

Category 4—Computers 198

Category 5—Telecommunications and “information security” 204

Category 6—Sensors and lasers 222

Category 7—Navigation and avionics 270

Category 8—Marine 285

Category 9—Aerospace and propulsion 292

Sensitive list of dual‑use goods and technologies 315

Very sensitive list of dual‑use goods and technologies 328

Schedule 1—Repeals 334

Defence and Strategic Goods List 1996 334

Part 1A—Preliminary

Division 1—Preliminary

1 Name

This instrument is the Defence and Strategic Goods List 2019.

1A Commencement

(1) Each provision of this instrument specified in column 1 of the table commences, or is taken to have commenced, in accordance with column 2 of the table. Any other statement in column 2 has effect according to its terms.

Commencement information
Column 1	Column 2	Column 3
Provisions	Commencement	Date/Details
1. The whole of this instrument	The day after this instrument is registered.	28 March 2019

Note: This table relates only to the provisions of this instrument as originally made. It will not be amended to deal with any later amendments of this instrument.

(2) Any information in column 3 of the table is not part of this instrument. Information may be inserted in this column, or information in it may be edited, in any published version of this instrument.

2 Authority

This instrument is made under paragraph 112(2A)(aa) of the Customs Act 1901.

2A Schedules

Each instrument that is specified in a Schedule to this instrument is amended or repealed as set out in the applicable items in the Schedule concerned, and any other item in a Schedule to this instrument has effect according to its terms.

Division 2—Simplified outline of the Defence and Strategic Goods List

The Defence and Strategic Goods List is divided in 2 Parts.

Part 1 of the List covers defence and related goods, that is goods and technologies designed or adapted for use by armed forces or goods that are inherently lethal. These goods include:

military goods, being goods or technology that is designed or adapted for military purposes, including their parts and accessories; and

non‑military lethal goods, being equipment that is inherently lethal, incapacitating or destructive, such as non‑military firearms, non‑military ammunition and commercial explosives and initiators.

Part 2 of the List covers those goods that have a dual use. Dual‑use 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 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 List is amended from time to time to reflect changes in the various multilateral non‑proliferation and export control regimes of which Australia is a member.

Division 3—Interpretation

3.1 Definitions

Terms in “quotation marks” are defined terms (see Division 4—Definitions). Words and terms that are defined and that appear in the Defence and Strategic Goods List without quotation marks are intended to take their ordinary dictionary meanings.

3.2 Notes

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.

3.3 Incorporated goods

The object of the controls contained in the Defence and Strategic Goods List should not be defeated by the export of any non‑controlled 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.

Note: 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 know‑how involved and other special circumstances which might establish the controlled component or components as the principal element of the goods being procured.

3.4 New and used goods

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

3.5 CAS numbers

In some instances, chemicals are listed by name and CAS number. The list applies to chemicals of the same structural formula (including hydrates) regardless of name or CAS number. CAS numbers are shown to assist in identifying a particular chemical or mixture, irrespective of nomenclature. CAS numbers cannot be used as unique identifiers because:

(a) some forms of the listed chemical have different CAS numbers; and

(b) mixtures containing a listed chemical may also have different CAS numbers.

3.6 Source code

“Source code” items are controlled either by “software” or by “software” and “technology” controls, except when such “source code” items are explicitly decontrolled.

3.7 Medical equipment

Equipment specially designed for medical end‑use that incorporates an item controlled in the Dual‑Use List is not controlled.

3.8 Nuclear technology note (NTN)

Note: To be read in conjunction with section E of Category 0.

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

3.82 “Technology” for the “development”, “production” or “use” of goods under control remains under control even when applicable to non‑controlled goods.

3.83 The approval of goods for export also authorises the export to the same end‑user of the minimum “technology” required for the installation, operation, maintenance and repair of the goods.

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

3.9 General technology note (GTN)

Note: This note applies to all technology controls in Categories 1 to 9 of the Dual‑Use List.

3.91 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.

3.92 “Technology” “required” for the “development”, “production” or “use” of goods under control remains under control even when applicable to non‑controlled goods.

3.93 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.

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

3.94 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.

3.10 General software note (GSN)

Note: This note applies to all software controls in the Defence and Strategic Goods List.

3.101 The Defence and Strategic Goods List does not control “software” which is any of the following:

(1) generally available to the public by being:

(a) sold from stock at retail selling points, without restriction, by means of:

1. over the counter transactions; or

2. mail order transactions; or

3. electronic transactions; or

4. telephone order transactions; and

(b) designed for installation by the user without further substantial support by the supplier;

Note: Entry (1) does not release “software” specified in Category 5 ‑ Part 2 (“Information Security”).

(2) “in the public domain”;

(3) the minimum necessary “object code” for the installation, operation, maintenance (checking) or repair of those items whose export has been authorised.

Note: Entry (3) does not release “software” controlled by Category 5 ‑ Part 2 (“Information Security”).

3.11 General “information security” note (GISN)

3.111 "Information security" items or functions should be considered against the provisions in Category 5 Part 2, even if they are components, "software" or functions of other items.

Division 4—Definitions

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

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

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

“Accuracy” (2 3 6 7 8), 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) is a minimum (single) element of the solid state array which has a photoelectric transfer function when exposed to light (electromagnetic) radiation.

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

Note: See Category 4, Technical Note.

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

“Aircraft” (1 6 7 9 ML8 ML10 ML14) means a fixed wing, swivel wing, rotary wing (helicopter), tilt rotor or tilt‑wing airborne vehicle.

Note: See also “civil aircraft”.

“Airship” (9) means a power‑driven airborne vehicle that is kept buoyant by a body of gas (usually helium, formerly hydrogen) which is lighter than air.

“All compensations available” (2) means after all feasible measures available to the manufacturer to minimise all systematic positioning errors for the particular machine‑tool 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.

Note: 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 528‑2001)

“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.

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

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

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

“Authentication” (5) means verifying the identity of a user, process or device, often as a prerequisite to allowing access to resources in an information system. This includes verifying the origin or content of a message or other information, and 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.

“Automated Command and Control Systems” (ML11) means electronic systems, through which information essential to the effective operation of the grouping, major formation, tactical formation, unit, ship, subunit or weapons under command is entered, processed and transmitted. This is achieved by the use of computer and other specialised hardware designed to support the functions of a military command and control organisation. The main functions of an automated command and control system are: the efficient automated collection, accumulation, storage and processing of information; the display of the situation and the circumstances affecting the preparation and conduct of combat operations; operational and tactical calculations for the allocation of resources among force groupings or elements of the operational order of battle or battle deployment according to the mission or stage of the operation; the preparation of data for appreciation of the situation and decision‑making at any point during operation or battle; computer simulation of operations.

“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’.

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

Note 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; and

(b) the common design and process technology; and

(c) the common basic characteristics.

“Basic scientific research” (GTN NTN ML22) 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 g or in metres per second squared (g or m/s²). (IEEE STD 528‑2001) (Micro g equals 1x10^‑6 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 528‑2001).

“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.

“Biological agents” (1 ML7) means pathogens or toxins, selected or modified (such as altering purity, shelf life, virulence, dissemination characteristics, or resistance to UV radiation) to produce casualties in humans or animals, degrade equipment or damage crops or the environment.

“Biopolymers” (ML7 ML22) means biological macromolecules as follows:

(a) enzymes for specific chemical or biochemical reactions;

(b) ‘Anti‑idiotypic’, ‘monoclonal’ or ‘polyclonal’ ‘antibodies’;

(c) specially designed or specially processed ‘receptors’.

Technical Notes:

1. ‘Anti‑idiotypic 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) 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).

"Circular Error Probable" ("CEP") (7) means, in a circular normal distribution, the radius of the circle containing 50% of the individual measurements being made, or the radius of the circle within which there is a 50% probability of being located.

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

“Circuit elements” (6) means a single active or passive functional part of an electronic circuit, such as one diode, one transistor, one resistor, one capacitor, etc.

“Circulation‑controlled anti‑torque 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 3 4 7 9 ML4 ML10) means those “aircraft” listed by designation in published airworthiness certification lists by the civil aviation authorities of one or more Wassenaar Arrangement Participating States to fly commercial civil internal and external routes or for legitimate civil, private or business use.

Note: See also “aircraft”.

“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.

“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, gallium‑aluminium 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 2806:1994).

“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.

“Cryptographic activation” (5) means any technique that activates or enables cryptographic capability of an item, by means of a secure mechanism implemented by the manufacturer of the item, where this mechanism is uniquely bound to either of the following:

(1) a single instance of the item;

(2) one customer, for multiple instances of the item.

Technical Notes:

1. ″Cryptographic activation″ techniques and mechanisms may be implemented as hardware, ″software″ or ″technology″.

2. Mechanisms for “cryptographic activation” can, for example, be serial member‑based licence keys or authentication instruments such as digitally signed certificates.

“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.

Note: “Cryptography” does not include ‘fixed’ data compression or coding techniques.

Technical Notes:

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

2. 'Fixed': the coding or compression algorithm cannot accept externally supplied parameters (e.g., cryptographic or key variables) and cannot be modified by the user.

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

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

“Deactivated firearm” (ML1) means a firearm that:

(a) was in a condition in which it could discharge shot, bullets or other projectiles by means of an explosive charge or a compressed gas; and

(b) has been rendered incapable of discharging shot, bullets or other projectiles by means of an explosive charge or a compressed gas; and

(c) cannot be returned to a condition in which it could discharge shot, bullets or other projectiles by means of an explosive charge or a compressed gas; and

(d) still has the appearance of a firearm, and could reasonably be taken to be a firearm.

Note: A firearm can be deactivated to the extent that it is incapable of being returned to its original firing condition, while keeping the appearance of a firearm. For the article to be incapable of being returned to its original firing condition, all major parts of the article must be destroyed, permanently incapacitated or permanently immobilised. This includes (but is not limited to) the bolt, barrel, gas system, receiver, trigger, sear or hammer, feed pawls and actuating arm or arms. This can be done by any of the following:

(a) fusion welding, which is welding material into the barrel, and welding of all the major parts of the firearm, in a way that cannot be reversed;

(b) sectioning, which is the machining or milling of all the major parts of the firearm in a way that cannot be reversed, exposing the internal mechanism;

(c) another method of treating the major parts that ensures that the parts are deactivated to the extent that the firearm is incapable of being returned to its original firing condition.

“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, wherein the principal mechanism is interdiffusion of atoms across the interface.

“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;

(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.

Note: See also “total digital transfer rate”.

“Discrete component” means a separately packaged “circuit element” with its own external connections.

“Electronic assembly” (2 3 4) 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.

Note 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.

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

“End‑effectors” (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.

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.

“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.

“Fibrous or filamentary materials” (0 1 2 8 9 ML13) 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”.

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, multi‑alkali photocathodes (S‑20 or S‑25), but not microchannel plate amplifiers.

"Fly‑by‑light system" (7) is a primary digital flight control system employing feedback to control the “aircraft” during flight, where the commands to the effectors/actuators are optical signals.

"Fly‑by‑wire system" (7) is primary digital flight control system employing feedback to control the “aircraft” during flight, where the commands to the effectors/actuators are electrical signals.

“Focal plane array” (6) means a linear or two‑dimensional 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 6) means a form of “spread spectrum” in which the transmission frequency of a single communication channel is made to change by a random or pseudo‑random sequence of discrete steps.

“Frequency switching time” (3) means the time (i.e., delay) taken by a signal when switched from an initial specified output frequency, to arrive at or within any of the following:

a. ±100 Hz of a final specified output frequency of less than 1 GHz; or

b. ±0.1 part per million of a final specified output frequency equal to or greater than 1 GHz.

“Fuel cell” (8 ML17) means an electrochemical device that converts chemical energy directly into Direct Current (DC) electricity by consuming fuel from an external source.

“Full Authority Digital Engine Control Systems” (“FADEC Systems”) (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.

“Fusible” (1) means capable of being cross‑linked or polymerised further (cured) by the use of heat, radiation, catalysts, etc., or that can be melted without pyrolysis (charring).

“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.

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

(a) accept data;

(b) process data, in both analogue and digital representations;

(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;

(d) not normally capable of being disassembled.

Note 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.

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

“Image enhancement” (4) means the processing of externally derived information‑bearing 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 “sub‑unit 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” (GSN GTN 5P2) 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”, “cryptographic activation”, ‘cryptanalysis’, protection against compromising emanations and computer security.

Note: ‘Cryptanalysis’ is the analysis of a cryptographic system or its inputs and outputs to derive confidential variables or sensitive data, including clear text. (ISO 7498‑2‑1988 (E), paragraph 3.3.18).

“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 semi‑cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.

“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.

“Interleaved Analogue‑to‑Digital Converter (ADC)” (3) means devices that have multiple ADC units that sample the same analogue input at different times such that when the outputs are aggregated, the analogue input has been effectively sampled and converted at a higher sampling rate.

“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.

Note: See also “magnetic gradiometer”.

“Intrusion software” (4) “Software” specially designed or modified to avoid detection by ‘monitoring tools’, or to defeat ‘protective countermeasures’, of a computer or network‑capable device, and performing any of the following:

(a) the extraction of data or information, from a computer or network‑capable device, or the modification of system or user data; or

(b) the modification of the standard execution path of a program or process in order to allow the execution of externally provided instructions.

Note 1: “Intrusion software” does not include any of the following:

(a) hypervisors, debuggers or Software Reverse Engineering (SRE) tools;

(b) digital Rights Management (DRM) “software”;

(c) “Software” designed to be installed by manufacturers, administrators or users, for the purposes of asset tracking or recovery.

Note 2: Network‑capable devices include mobile devices and smart meters.

Technical Notes:

1. ‘Monitoring tools’: “software” or hardware devices, that monitor system behaviours or processes running on a device. This includes antivirus (AV) products, end point security products, Personal Security Products (PSP), Intrusion Detection Systems (IDS), Intrusion Prevention Systems (IPS) or firewalls.

2. ‘Protective countermeasures’: techniques designed to ensure the safe execution of code, such as Data Execution Prevention (DEP), Address Space Layout Randomisation (ASLR) or sandboxing.

“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 1 2 3 5P1 6 7 8 9 ML5 ML9 ML19) is an item that produces spatially and temporally coherent light through amplification by stimulated emission of radiation.

“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.

"Library" (parametric technical database) (1 ML17) is a collection of technical information, reference to which may enhance the performance of relevant systems, equipment or components.

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

“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;

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

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.

Note: 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.

“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 10360‑2).

“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.

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.

Note 1: The “microprocessor microcircuit” normally does not contain integral user‑accessible storage, although storage present on‑the‑chip may be used in performing its logic function.

Note 2: This includes chip sets which are designed to operate together to provide the function of a “microprocessor microcircuit”.

“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 register.

“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 so‑called ‘chip’; and

(b) can be considered as indivisibly associated; and

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

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.

"Monolithic Microwave Integrated Circuit" ("MMIC") (3 5) means a "monolithic integrated circuit" that operates at microwave or millimeter wave frequencies.

“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”.

“Multiple channel Analogue‑to‑Digital Converter (ADC)” (3) means devices that integrate more than one ADC, designed so that each ADC has a separate analogue input.

“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.

“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 2382:2015).

“Object code” (GSN) 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.

"Operations, Administration or Maintenance" ("OAM") (5) means performing one or more of the following tasks:

(a) establishing or managing any of the following:

(1) accounts or privileges of users or administrators;

(2) settings of an item;

(3) authentication data in support of the tasks described in paragraphs a.1. or a.2.;

(b) monitoring or managing the operating condition or performance of an item;

(c) managing logs or audit data in support of any of the tasks described in paragraphs (a) or (b).

Note: "OAM" does not include any of the following tasks or their associated key management functions:

(a) provisioning or upgrading any cryptographic functionality that is not directly related to establishing or managing authentication data in support of the tasks described in paragraphs a.1. or a.2. above;

(b) performing any cryptographic functionality on the forwarding or data plane of an item.

“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) electro‑optical 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 ampere‑turns 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 cross‑section of the coil (comprising the superconducting filaments, the metallic matrix in which the superconducting filaments are embedded, the encapsulating material, any cooling channels, etc.).

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

“Personal area network” (5) means a data communication system having all of the following characteristics:

(a) allows an arbitrary number of independent or interconnected ‘data devices’ to communicate directly with each other;

(b) is confined to the communication between devices within the immediate vicinity of an individual person or device controller (e.g., single room, office, or automobile, and their nearby surrounding spaces).

Technical Note:

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

“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.

“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(s)” (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 oxidisers 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 oxidisers 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 quantum‑mechanical properties of a physical system (including those physical properties explicitly governed by quantum optics, quantum field theory, or quantum electrodynamics).

“Radar frequency agility” (6) means any technique which changes, in a pseudo‑random 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 pseudo‑random coding.

“Radiant sensitivity” (6) Radiant sensitivity (mA/W) = 0.807 x (wavelength in nm) x Quantum Efficiency (QE)

Technical Note:

QE is usually expressed as a percentage; however, for the purposes of this formula QE is expressed as a decimal number less than one, e.g., 78% is 0.78.

“Real time processing” (6) 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 non‑operating periods occur between measurements. (Reference: IEEE STD 528‑2001 (one sigma standard deviation)).

“Required” (GTN 1 5 6 7 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.

“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.

Technical Note:

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 point‑to‑point 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 servo‑devices which may include stepping motors;

(d) has “user‑accessible 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. Non‑servo‑controlled 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.

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

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

“Run‑out” (2) (out‑of‑true 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 230/1‑1986, paragraph 5.61).

“Sample rate” (3) means for an Analogue‑to‑Digital Converter (ADC) the maximum number of samples that are measured at the analogue input over a period of one second, except for oversampling ADCs. For oversampling ADCs the “sample rate” is taken to be its output word rate. “Sample rate” may also be referred to as sampling rate, usually specified in Mega Samples Per Second (MSPS) or Giga Samples Per Second (GSPS), or conversion rate, usually specified in Hertz (Hz).

“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 input‑output data obtained by varying the input cyclically over the input range.

“Signal analysers” (3) mean apparatus capable of measuring and displaying basic properties of the single‑frequency components of multi‑frequency signals.

“Signal processing” (3 4 5 6) means the processing of externally derived information‑bearing 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.

“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 ML11) means active and passive satellites and space probes.

“Spacecraft bus” (9) is equipment that provides the support infrastructure of the "spacecraft" and location for the "spacecraft payload".

“Spacecraft payload” (9) is equipment, attached to the "spacecraft bus", designed to perform a mission in space (e.g., communications, observation, science).

“Space qualified” (3 6 7 ML19) refers to products designed, manufactured, or qualified through successful testing, for operation at altitudes greater than 100 km above the surface of the Earth.

Note: A determination that a specific item is “space‑ qualified” by virtue of testing does not mean that other items in the same production run or model series are “space‑qualified” if not individually tested.

“Special fissile material” (0) means plutonium‑239, uranium‑233, “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)%.

“Spinning mass gyros” (7) “Spinning mass gyros” are gyros which use a continually rotating mass to sense angular motion.

“Spread spectrum” (5) means the technique whereby energy in a relatively narrow‑band 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.

Technical Note:

For gyroscopes, "stability" can be estimated by determining the Allan variance noise‑analysis value at the integration period (i.e., sample time) consistent with the stated measurement period, which may include extrapolating the Allan variance noise analysis beyond the instability point into the rate random walk or rate ramp regions to an integration period consistent with the stated measurement period (Reference: IEEE Std 952‑1997 [R2008]). Allan variance noise analysis is often used to characterise MicroElectroMechanical Systems (MEMS) gyroscopes, and is applicable to other gyroscopes, such as Ring Laser Gyroscopes (RLGs) and Fibre Optic Gyroscopes (FOGs).

“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 State Mode” (9) 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.

“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.

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

Note 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” (3 6) means monolithic compounds with dimensions suitable for the production of optical elements such as mirrors or optical windows.

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

“Superalloys” (2 9) mean nickel‑, cobalt‑ or iron‑base 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.

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.

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

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

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’. Specified “technology” for the Dual‑Use List is defined in the General Technology Note and in the Dual‑Use List. Specified “technology” for the Munitions List is defined in ML22.

Note 1: ‘Technical assistance’ may take forms such as instruction, skills, training, working knowledge and consulting services and may involve the transfer of ‘technical data’.

Note 2: ‘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, read‑only memories.

“Three dimensional integrated circuit” (3) means collection of semiconductor dies or active device layers, integrated together, and having through semiconductor via connections passing completely through an interposer, substrate, die or layer to establish interconnections between the device layers. An interposer is an interface that enables electrical connections.

“Tilting spindle” (2) means a tool‑holding 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 1‑1/e times the final value (i.e., 63% of the final value).

“Time to steady‑state registration” (6) (also referred to as the gravity meter’s response time) is the time over which the disturbing effects of platform‑induced acceleration (high frequency noise) are reduced.

“Tip shroud” (9) means a stationary ring component (solid or segmented) attached to the inner surface of the engine turbine casing or a feature at the outer tip of the turbine blade, which primarily provides a gas seal between the stationary and rotating components.

“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.

Note: 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”.

“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”.

“Unidirectional positioning repeatability” (2) means the smaller of values R↑ and R↓ (forward and backward), as defined by 3.21 of ISO 230‑2:2014 or national equivalents, of an individual machine tool axis.

“Unmanned aerial vehicle” (“UAV”) (9 ML10) 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 Dual‑Use List) means operation, installation (including on‑site installation), maintenance (checking), repair, overhaul and refurbishing.

“User‑accessible 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.

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

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

Division 5—Acronyms and abbreviations

5.1 An acronym or abbreviation, when used as a defined term, will be found in Division 4 (Definitions).

Acronym or abbreviation	Meaning
ABEC	Annular Bearing Engineers Committee
ADC	Analogue‑to‑Digital Converter
AGMA	American Gear Manufacturers’ Association
AHRS	Attitude and Heading Reference Systems
AISI	American Iron and Steel Institute
ALE	Atomic Layer Epitaxy
ALU	Arithmetic Logic Unit
ANSI	American National Standards Institute
APP	Adjusted Peak Performance
APU	Auxiliary Power Unit
ASTM	the American Society for Testing and Materials
ATC	Air Traffic Control
AVLIS	Atomic Vapour Laser Isotope Separation
BJT	Bipolar Junction Transistors
BPP	Beam Parameter Product
BSC	Base Station Controller
C3I	Command, Communications, Control & Intelligence
CAD	Computer‑Aided‑Design
CAS	Chemical Abstracts Service
CCD	Charge Coupled Device
CDU	Control and Display Unit
CEP	Circular Error Probable
CMM	Coordinate Measuring Machine
CMOS	Complementary Metal Oxide Semiconductor
CNTD	Controlled Nucleation Thermal Deposition
CPLD	Complex Programmable Logic Device
CPU	Central Processing Unit
CRISLA	Chemical Reaction by Isotope Selective Laser Activation.
CVD	Chemical Vapour Deposition
CW	Chemical Warfare
CW (for lasers)	Continuous Wave
DAC	Digital‑to‑Analogue Converter
DANL	Displayed Average Noise Level
DBRN	Data‑Base Referenced Navigation
DDS	Direct Digital Synthesizer
DEW	Directed Energy Weapon Systems
DMA	Dynamic Mechanical Analysis
DME	Distance Measuring Equipment
DMOSFET	Diffused Metal Oxide Semiconductor Field Effect Transistor
DS	Directionally Solidified
EB	Exploding Bridge
EB‑PVD	Electron Beam Physical Vapour Deposition
EBW	Exploding Bridge Wire
ECM	Electro‑Chemical Machining
ECR	Electron Cyclotron Resonance
EDM	Electrical Discharge Machines
EEPROM	Electrically Erasable Programmable Read Only Memory
EFI	Exploding Foil Initiators
EIRP	Effective Isotropic Radiated Power
EMC	Electromagnetic Compatibility
EMCDB	Elastomer Modified Cast Double Based Propellants
ERF	Electrorheological Finishing
ERP	Effective Radiated Power
ETO	Emitter Turn‑Off Thyristor
ETT	Electrical Triggering Thyristor
FADEC	Full Authority Digital Engine Control
FFT	Fast Fourier Transform
FPGA	Field Programmable Gate Array
FPIC	Field Programmable Interconnect
FPLA	Field Programmable Logic Array
FPO	Floating Point Operation
FWHM	Full‑Width Half‑Maximum
GLONASS	Global Navigation Satellite System
GNSS	Global Navigation Satellite System
GPS	Global Positioning System
GSM	Global System for Mobile Communications
GTO	Gate Turn‑off Thyristor
HBT	Hetero‑Bipolar Transistors
HEMT	High Electron Mobility Transistors
ICAO	International Civil Aviation Organisation
IEC	International Electro‑technical Commission
IED	Improvised Explosive Device
IEEE	Institute of Electrical and Electronic Engineers
IFOV	Instantaneous‑Field‑of‑View
IGBT	Insulated Gate Bipolar Transistor
IGCT	Integrated Gate Commutated Thyristor
IHO	International Hydrographic Organization
ILS	Instrument Landing System
IMU	Inertial Measurement Unit
INS	Inertial Navigation System
IP	Internet Protocol
IRS	Inertial Reference System
IRU	Inertial Reference Unit
ISA	International Standard Atmosphere
ISAR	Inverse Synthetic Aperture Radar
ISO	International Organization for Standardization
ITU	International Telecommunication Union
JT	Joule‑Thomson
LIDAR	Light Detection and Ranging
LIDT	Laser Induced Damage Threshold
LOA	Length Overall
LRU	Line Replaceable Unit
LTT	Light Triggering Thyristor
LVDT	Linear Variable Differential Transformer
Mach	Ratio of speed of an object to speed of sound (after Ernst Mach)
MLIS	Molecular Laser Isotopic Separation
MLS	Microwave Landing Systems
MMIC	Monolithic Microwave Integrated Circuit
MOCVD	Metal Organic Chemical Vapour Deposition
MOSFET	Metal‑Oxide‑Semiconductor Field Effect Transistor
MPM	Microwave Power Module
MRAM	Magnetic Random Access Memory
MRF	Magnetorheological Finishing
MRF	Minimum Resolvable Feature size
MRI	Magnetic Resonance Imaging
MTBF	Mean‑Time‑Between‑Failures
MTTF	Mean‑Time‑To‑Failure
NA	Numerical Aperture
NBC	Nuclear, Biological and Chemical
NDT	Non‑Destructive Test
NEQ	Net Explosive Quantity
OAM	Operations, Administration or Maintenance
OSI	Open Systems Interconnection
PAI	Polyamide‑imides
PAR	Precision Approach Radar
PCL	Passive Coherent Location
PIN	Personal Identification Number
PMR	Private Mobile Radio
Ppm	Parts per million
PVD	Physical Vapour Deposition
QAM	Quadrature‑Amplitude‑Modulation
RAP	Reactive Atom Plasmas
RF	Radio Frequency
RNC	Radio Network Controller
RPV	Remotely Piloted Air Vehicle
S‑FIL	Step and Flash Imprint Lithography
SAR	Synthetic Aperture Radar
SAS	Synthetic Aperture Sonar
SC	Single Crystal
SCR	Silicon Controlled Rectifier
SFDR	Spurious Free Dynamic Range
SHPL	Super High Powered Laser
SLAR	Sidelooking Airborne Radar
SOI	Silicon‑on‑Insulator
SPLD	Simple Programmable Logic Device
SQUID	Superconducting Quantum Interference Device
SRA	Shop Replaceable Assembly
SRAM	Static Random Access Memory
SSB	Single Sideband
SSR	Secondary Surveillance Radar
SSS	Side Scan Sonar
TCSEC	Trusted Computer System Evaluation Criteria
TE‑PVD	Thermal Evaporation‑Physical Vapour Deposition
TIR	Total Indicated Reading
TVR	Transmitting Voltage Response
UAV	Unmanned Arial Vehicle
UPR	Unidirectional Positioning Repeatability
UTS	Ultimate Tensile Strength
VJFET	Vertical Junction Field Effect Transistor
VOR	Very High Frequency Omni‑directional Range
WLAN	Wireless Local Area Network
YAG	Yttrium/Aluminium Garnet

Part 1—Munitions list

ML1. Smooth‑bore 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:

Note: ML1. does not apply to:

a. Firearms specially designed for dummy ammunition and which are incapable of discharging a projectile;

b. Firearms specially designed to launch tethered projectiles having no high explosive charge or communications link, to a range of less than or equal to 500 m.;

c. Weapons using non‑centre fire cased ammunition and which are not of the fully automatic firing type;

d. “Deactivated firearms”.

a. Rifles and combination guns, handguns, machine, sub‑machine and volley guns;

Note: ML1.a. does not apply to the following:

a. Rifles and combination guns, manufactured earlier than 1938;

b. Reproductions of rifles and combination guns the originals of which were manufactured earlier than 1890;

c. Handguns, volley guns and machine guns, manufactured earlier than 1890, and their reproductions.

d. Rifles or handguns, specially designed to discharge an inert projectile by compressed air or CO₂

b. Smooth‑bore weapons as follows:

1. Smooth‑bore weapons specially designed for military use;

2. Other smooth‑bore weapons as follows:

a. Fully automatic type weapons;

b. Semi‑automatic or pump‑action type weapons;

Note: ML1.b.2. does not apply to weapons specially designed to discharge an inert projectile by compressed air or CO₂.

Note: ML1.b. does not apply to the following:

a. Smooth‑bore weapons manufactured earlier than 1938;

b. Reproductions of smooth‑bore weapons, the originals of which were manufactured earlier than 1890.

c. Smooth‑bore weapons used for hunting or sporting purposes. These weapons must not be specially designed for military use or of the fully automatic firing type;

d. Smooth‑bore weapons specially designed for any of the following:

1. Slaughtering of domestic animals;

2. Tranquilizing of animals;

3. Seismic testing;

4. Firing of industrial projectiles; or

5. Disrupting Improvised Explosive Devices (IEDs).

N.B.: For disruptors, see ML4. and 1A006. on the Dual‑Use List.

c. Weapons using caseless ammunition;

d. Accessories designed for arms specified by ML1.a., ML1.b. or ML1.c., as follows:

1. Detachable cartridge magazines;

2. Sound suppressors or moderators;

3. Special gun‑mountings;

4. Flash suppressors;

5. Optical weapon‑sights with electronic image processing;

6. Optical weapon‑sights specially designed for military use.

ML2. Smooth‑bore 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, anti‑tank weapons, projectile launchers, military flame throwers, rifles, recoilless rifles, smooth‑bore 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 specified by ML2.a.

Note 2: ML2.a. does not apply to weapons as follows:

a. Rifles, smooth‑bore weapons and combination guns, manufactured earlier than 1938;

b. Reproductions of rifles, smooth‑bore weapons and combination guns, the originals of which were manufactured earlier than 1890;

c. Guns, howitzers, cannons, mortars, manufactured earlier than 1890;

d. Smooth‑bore weapons used for hunting or sporting purposes. These weapons must not be specially designed for military use or of the fully automatic firing type;

e. Smooth‑bore weapons specially designed for any of the following:

1. Slaughtering of domestic animals;

2. Tranquilizing of animals;

3. Seismic testing;

4. Firing of industrial projectiles; or

5. Disrupting Improvised Explosive Devices (IEDs);

N.B. For disruptors, see ML4. and 1A006. on the Dual‑Use List.

f. Hand‑held projectile launchers specially designed to launch tethered projectiles having no high explosive charge or communications link, to a range of less than or equal to 500 m.

b. Smoke, gas and pyrotechnic projectors or generators, specially designed or modified for military use;

Note: ML2.b. does not apply to signal pistols.

c. Weapons sights and weapon sight mounts, having all of the following:

1. Specially designed for military use; and

2. Specially designed for weapons specified by ML2.a.;

d. Mountings specially designed for the weapons specified by ML2.a.

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

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

b. Fuse setting devices specially designed for ammunition specified by ML3.a.

Note 1: Specially designed components specified by ML3. 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 one‑time operational output;

d. Combustible cases for charges;

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

Note 2: ML3.a. does not apply to any of the following:

a. Ammunition crimped without a projectile (blank star);

b. Dummy ammunition with a pierced powder chamber;

c. Other blank and dummy ammunition, not incorporating components designed for live ammunition; or

d. Components specially designed for blank or dummy ammunition, specified in this Note 2.a., b. or c.

Note 3: ML3.a. does not apply to 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, and specially designed components therefor:

N.B. 1: For guidance and navigation equipment, see ML11.

N.B. 2: For Aircraft Missile Protection Systems (AMPS), see ML4.c.

a. Bombs, torpedoes, grenades, smoke canisters, rockets, mines, missiles, depth charges, demolition‑charges, demolition‑devices, demolition‑kits, “pyrotechnic” devices, cartridges and simulators (i.e., equipment simulating the characteristics of any of these items), specially designed for military use;

Note: ML4.a. includes:

a. smoke grenades, fire bombs, incendiary bombs and explosive devices;

b. missile rocket nozzles and re‑entry vehicle nosetips.

b. Equipment having all of the following:

1. Specially designed for military use; and

2. Specially designed for ‘activities’ relating to any of the following:

a. Items specified by ML4.a.; or

b. Improvised Explosive Devices (IEDs).

Technical Note:

For the purpose of ML4.b.2., ‘activities’ applies to handling, launching, laying, controlling, discharging, detonating, activating, powering with one‑time operational output, decoying, jamming, sweeping, detecting, disrupting or disposing.

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 hand‑held devices limited by design solely to the detection of metal objects and incapable of distinguishing between mines and other metal objects.

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 100‑400 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 surface‑to‑air missiles; and

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

9E002 “Technology” according to the General Technology Note for the “production” of equipment specified by 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 stress‑rupture life exceeding 400 hours at 1,273 K (1,000°C) at a stress of 200 MPa, based on the average property values;

Technical Note:

For the purposes of 9E003.a.1., stress‑rupture life testing is typically conducted on a test specimen.

2. Combustors having any of the following:

a.‘Thermally decoupled liners’ designed to operate at ‘combustor exit temperature’ exceeding 1,883 K (1,610°C);

b.Non‑metallic liners;

c.Non‑metallic shells; or

d.Liners designed to operate at ‘combustor exit temperature’ exceeding 1,883 K (1,610°C) and having holes that meet the parameters specified by 9E003.c.;

Note: The “required” “technology” for holes in 9E003.a.2. is limited to the derivation of the geometry and location of the holes.

Technical Notes:

1.'Thermally decoupled liners' are liners that feature at least a support structure designed to carry mechanical loads and a combustion facing structure designed to protect the support structure from the heat of combustion. The combustion facing structure and support structure have independent thermal displacement (mechanical displacement due to thermal load) with respect to one another, i.e. they are thermally decoupled.

2.‘Combustor exit temperature’ is the bulk average gas path total (stagnation) temperature between the combustor exit plane and the leading edge of the turbine inlet guide vane (i.e., measured at engine station T40 as defined in SAE ARP 755A) when the engine is running in a “steady state mode” of operation at the certificated maximum continuous operating temperature.

N.B.: See 9E003.c. for “technology” “required” for manufacturing cooling holes.

3. Components that are any of the following:

a. Manufactured from organic "composite" materials designed to operate above 588 K (315°C);

b. Manufactured from any of the following:

1. Metal "matrix" "composites" reinforced by any of the following:

a. Materials specified by 1C007.;

b. "Fibrous or filamentary materials" specified by 1C010.; or

c. Aluminides specified by 1C002.a; or

2. Ceramic "matrix" "composites" specified by 1C007.; or

c. Stators, vanes, blades, tip seals (shrouds), rotating blings, rotating blisks, or 'splitter ducts', that are all of the following:

1. Not specified by 9E003.a.3.a.;

2. Designed for compressors or fans; and

3. Manufactured from material specified by 1C010.e. with resins specified by 1C008.;

Technical Note:

A 'splitter duct' performs the initial separation of the air‑mass flow between the bypass and core sections of the engine.

4. Uncooled turbine blades, vanes or "tip‑shrouds", designed to operate at a 'gas path temperature' of 1,373 K (1,100°C) or more;

5. Cooled turbine blades, vanes, “tip‑shrouds” other than those described in 9E003.a.1., designed to operate at a ‘gas path temperature’ of 1,693 K (1,420°C) or more;

Technical Note:

‘Gas path temperature’ is the bulk average gas path total (stagnation) temperature at the leading edge plane of the turbine component when the engine is running in a ‘steady state mode’ of operation at the certificated or specified maximum continuous operating temperature.

6. Airfoil‑to‑disk blade combinations using solid state joining;

7. Gas turbine engine components using “diffusion bonding” “technology” specified by 2E003.b.;

8. ‘Damage tolerant’ gas turbine engine rotor components using powder metallurgy materials specified by 1C002.b.; or

Technical Note:

‘Damage tolerant’ components are designed using methodology and substantiation to predict and limit crack growth.

9. Not used;

10. Not used;

11. Hollow fan blades;

b. “Technology” “required” for the “development” or “production” of any of the following:

1. Wind tunnel aero‑models equipped with non‑intrusive 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 manufacturing cooling holes, in gas turbine engine components incorporating any of the “technologies” specified by 9E003.a.1., 9E003.a.2. or 9E003.a.5., and having any of the following:

1. Having all of the following:

a. Minimum ‘cross‑sectional area’ less than 0.45 mm²;

b. ‘Hole shape ratio’ greater than 4.52; and

c. ‘Incidence angle’ equal to or less than 25°; or

2. Having all of the following:

a. Minimum ‘cross‑sectional area’ less than 0.12 mm²;

b. ‘Hole shape ratio’ greater than 5.65; and

c. ‘Incidence angle’ more than 25°;

Note: 9E003.c. does not apply to “technology” for manufacturing constant radius cylindrical holes that are straight through and enter and exit on the external surfaces of the component.

Technical Notes:

1. For the purposes of 9E003.c., the ‘cross‑sectional area’ is the area of the hole in the plane perpendicular to the hole axis.

2. For the purposes of 9E003.c., ‘hole shape ratio’ is the nominal length of the axis of the hole divided by the square root of its minimum ‘cross‑sectional area’.

3. For the purposes of 9E003.c., ‘incidence angle’ is the acute angle measured between the plane tangential to the aerofoil surface and the hole axis at the point where the hole axis enters the aerofoil surface.

4. Methods for manufacturing holes in 9E003.c. include “laser” beam machining, water jet machining, Electro‑Chemical Machining (ECM) or Electrical Discharge Machining (EDM).

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 any 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 centre‑line 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 by 1C007:

a. Cylinder liners;

b. Pistons;

c. Cylinder heads; and

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 single‑stage 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.

h. “Technology” for gas turbine engine “FADEC systems” as follows:

1. “Development” “technology” for deriving the functional requirements for the components necessary for the “FADEC system” to regulate engine thrust or shaft power (e.g. feedback sensor time constants and accuracies, fuel valve slew rate);

2. “Development” or “production” “technology” for control and diagnostic components unique to the “FADEC system” and used to regulate engine thrust or shaft power;

3. “Development” “technology” for the control law algorithms, including “source code”, unique to the “FADEC system” and used to regulate engine thrust or shaft power.

Note: 9E003.h. does not apply to technical data related to engine‑“aircraft” integration required by civil aviation authorities of one or more Wassenaar Arrangement Participating States to be published for general airline use (e.g., installation manuals, operating instructions, instructions for continued airworthiness) or interface functions (e.g., input/output processing, airframe thrust or shaft power demand).

i. “Technology” for adjustable flow path systems designed to maintain engine stability for gas generator turbines, fan or power turbines, or propelling nozzles, as follows:

1. “Development” “technology” for deriving the functional requirements for the components that maintain engine stability;

2. “Development” or “production” “technology” for components unique to the adjustable flow path system and that maintain engine stability;

3. “Development” “technology” for the control law algorithms, including “source code”, unique to the adjustable flow path system and that maintain engine stability.

Note: 9E003.i. does not apply to "technology" for any of the following:

a. Inlet guide vanes;

b. Variable pitch fans or prop‑fans;

c. Variable compressor vanes;

d. Compressor bleed valves; or

e. Adjustable flow path geometry for reverse thrust.

j. "Technology" "required" for the "development" of wing‑folding systems designed for fixed‑wing “aircraft” powered by gas turbine engines.

N.B.: For "technology" "required" for the "development" of wing‑folding systems designed for fixed‑wing “aircraft” specified by ML10., see ML22.

9E101 a. “Technology” according to the General Technology Note for the “development” of goods specified by 9A101, 9A102, 9A104 to 9A111 or 9A115 to 9A121.

b. “Technology” according to the General Technology Note for the “production” of ‘UAV’s specified by 9A012 or goods specified by 9A101, 9A102, 9A104 to 9A111 or 9A115 to 9A121.

Technical Note:

In 9E101.b. ‘UAV’ means unmanned aerial vehicle systems capable of a range exceeding 300 km.

9E102 “Technology” according to the General Technology Note for the “use” of space launch vehicles specified by 9A004, goods specified by 9A005 to 9A011, ‘UAV’s specified by 9A012 or goods specified by 9A101, 9A102, 9A104 to 9A111, 9A115 to 9A121, 9B105, 9B106, 9B115 to 9B117, 9D101 or 9D103.

Technical Note:

In 9E102, ‘UAV’ means unmanned aerial vehicle systems capable of a range exceeding 300 km.

Sensitive list of dual‑use goods and technologies

Note: This list contains a sub‑set of the items listed in Categories 1 to 9 of the Part 2 Dual‑Use List. 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 or supply of the following sensitive goods or technologies.

N.B.: Where abbreviated entries are used, see the Dual‑Use List for full details. Text that differs from that in the Dual‑Use List is shaded.

Category 1	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
1A002.a.1	“Composite” structures or laminates made from an organic “matrix” and “fibrous or filamentary materials” specified by 1C010.c. or 1C010.d.
1C001	Materials specially designed for absorbing electromagnetic radiation...
1C007.c.	Ceramic‑“matrix” “composite” materials...
1C007.d.	Not used
1C010.c. & 1C010.d.	“Fibrous or filamentary materials”...
1C012	Materials as follows...
1C101	Materials or devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures; other than those specified by 1C001, usable in ‘missiles’, ‘missile’ subsystems or unmanned aerial vehicles specified by 9A012. Note: 1C101 does not apply to 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, other than those specified in the Munitions List, 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.
1D002	“Software” for the “development” of organic “matrix”, metal “matrix” or carbon “matrix” laminates or “composites” specified by this List.
1D103	“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 specified by 1A002 or 1C of this List.
1E002.e. & 1E002.f.	Other “technology”...
1E101	“Technology” according to the GTN for the “use” of goods specified by 1C101 or 1D103.
1E102	“Technology” according to the General Technology Note for the “development” of “software” specified by 1D101 or 1D103.
1E201	“Technology” according to the GTN for the “development” of “software” specified by 1D103.
Category 2	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
2B001.a	Not used since 2002
2B001.b	Not used since 2002
2B001.d	Not used since 2002
2B001.f	Not used since 2002
2B003	Not used since 2002
2D001	“Software”, other than that specified by 2D002, specially designed for the “development” or “production” of equipment as follows: a. Specified by 2B001.a., 2B001.b.1., or 2B001.b.2., and having a “unidirectional positioning repeatability” equal to or less (better) than 0.9 µm along one or more linear axis; b. Specified by 2B001.b.3., 2B001.d., 2B001.f. or 2B003.
2E001	“Technology” according to the General Technology Note for the “development” of equipment or “software” as follows: a. Equipment specified by 2B001.a., 2B001.b.1. or 2B001.b.2., and having a “unidirectional positioning repeatability” equal to or less (better) than 0.9 µm along one or more linear axis; b. Equipment specified by 2B001.b.3., 2B001.d., 2B001.f. or 2B003.; c. “Software” specified by 2D. of this List;
2E002	“Technology” according to the General Technology Note for the “production” of equipment as follows: a. Specified by 2B001.a., 2B001.b.1. or 2B001.b.2., and having a “unidirectional positioning repeatability” equal to or less (better) than 0.9 µm along one or more linear axis; b. Specified by 2B001.b.3., 2B001.d., 2B001.f. or 2B003.
Category 3	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
3A002.g.1	Atomic frequency standards… “Space‑qualified”
3A229	High‑current pulse generators, as follows… N.B.: See also ML4, ML909
3A232	Multipoint initiation systems, other than those specified by 1A007, as follows… N.B.: See also ML4
3B001.a.2	Not used
3D001.	“Software” specially designed for the “development” or “production” of equipment specified by 3A002.g. of this List.
3E001	“Technology” according to the General Technology Note for the “development” or “production” of equipment specified by 3A of this List.
3E201	“Technology” according to the General Technology Note for the “use” of equipment specified by 3A229 or 3A232.
Category 4	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
4A001.a.2.	Electronic computers...radiation hardened…
4A003.b.	Not used since 2002
4A003.c.	Not used since 2001
4D001	“Software” specially designed for the “development” or “production” of equipment specified by 4A of this List or for the “development” or “production” of “digital computers” having an ‘Adjusted Peak Performance’ (‘APP’) exceeding 16 Weighted TeraFLOPS (WT).
4E001	“Technology” according to the General Technology Note for the “development” or “production” of any of the following equipment or “software”: a. Equipment specified by 4.A. of this List; b. “Digital computers” having an ‘Adjusted Peak Performance’ (‘APP’) exceeding 16 Weighted TeraFLOPS (WT); or c. “Software” specified by 4.D. of this List.
Category 5	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
Part 1
5A001.b.3.	Being radio equipment…
5A001.b.5.	Being digitally controlled radio receivers…
5A001.h.			Counter Improvised Explosive Device (IED) equipment and related equipment...
5B001.a.	Equipment and specially designed components or accessories therefor, specially designed for the “development” or “production” of equipment, functions or features in 5A001 of this List.
5D001.a.	“Software” specially designed for the “development” or “production” of equipment, functions or features, specified by 5A001 of this List.
5D001.b.	Not used.
5E001.a.	“Technology” according to the General Technology Note for the “development” or “production” of equipment, functions or features specified by 5A001 or “software” specified by 5D001.a. of this List.
Part 2	None
Category 6	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
6A001.a.1.b.		Systems or transmitting and receiving arrays, designed for object detection or location, 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… 3. Sound pressure level exceeding 235 dB… 4. Forming beams of… 5. Designed to operate… 6. Designed to withstand...
6A001.a.1.e.	Active individual sonars…
6A001.a.2.a.1.	Hydrophones…Incorporating…
6A001.a.2.a.2.	Hydrophones…Incorporating flexible assemblies…
6A001.a.2.a.3.	Hydrophones…Having any…
6A001.a.2.a.5.	Hydrophones…Designed to operate…
6A001.a.2.a.6	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 hydrophone arrays 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.	“Space‑qualified” solid‑state detectors…
6A002.a.1.d.	“Space‑qualified” “focal plane arrays”….
6A002.a.2.a.	Image intensifier tubes … 1. A peak response… 2. Electron image amplification… 3. Photocathodes, as follows: a. Multialkali photocathodes (e.g., S‑20 and S‑25) having a luminous sensitivity exceeding 700 µA/lm; b. GaAs or GaInAs photocathodes; c. Other “III/V compound” semiconductor photocathodes.
6A002.a.2.b.	Image intensifier tubes…
6A002.a.3.	Non‑“space‑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 delay‑and‑integration 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 non‑scanning 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 Aluminium 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 (1‑dimensional) “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 non‑linear (2‑dimensional) “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 3. Solid‑state detectors having the characteristics listed in 6A002.a.1.;
6A002.e.	Not used N.B.: Entry moved to 6A002.a.1.d. in 2008.
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;
Note: 6A003.b.3. does not apply to imaging cameras specially designed or modified for underwater use.
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; or
c. Incorporating “focal plane arrays” listed in 6A002.a.3.g. of this List.
6A003.b.4.	Note 1 ...
Note 2 ...
Note 3 ...
Note 4 ...
Note 5: 6A003.b.4.c. does not apply to imaging cameras specially designed or modified for underwater use.
6A003.b.5.	Imaging cameras incorporating solid‑state detectors specified by 6A002.a.1.;
6A004.c.	“Space‑qualified” components for optical systems…
6A004.d.	Optical control equipment…
6A006.a.	Not used
6A006.a.1.	“Magnetometers”… Using “superconductive” (SQUID) “technology”…
6A006.a.2.	“Magnetometers” … Using optically pumped or nuclear precession (proton/Overhauser) “technology” having a ‘sensitivity’ lower (better) than 2pT rms per square root Hz;
6A006.c.1.	“Magnetic gradiometers” using multiple “magnetometers” specified by 6A006.a.1. or 6A006.a.2. of this List;
6A006.d.	“Compensation systems” for the following:
1. Magnetic sensors specified by 6A006.a.2 and using optically pumped or nuclear precession (proton/Overhauser) “technology” that will permit these sensors to realise a ‘sensitivity’ lower (better) than 2 pT rms per square root Hz.
2. Underwater electric field sensors specified by 6A006.b.
3. “Magnetic gradiometers” specified by 6A006.c. that will permit these sensors to realise a ‘sensitivity’ lower (better) than 3 pT/m rms per square root Hz.
6A006.e.	Underwater electromagnetic receivers incorporating “magnetometers” specified by 6A006.a.1. or 6A006.a.2. of this List.
6A006.g.	Not used
6A006.h.	Not used
6A008.d.	Radar systems…Capable of…
6A008.h.	Radar systems…Employing processing…
6A008.k.	Radar systems…Having “signal processing”…
6A008.l.3.	Not used
6B008	Pulse radar cross‑section…
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 specified by 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 specified by 6A or 6B of this List.
Category 7	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
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), except “guidance sets” designed for missiles with a range under 300 km or manned aircraft.
7B103	Test, calibration or alignment equipment specially designed for equipment specified by 7A117 above. Note: 7B001 does not apply to test, calibration or alignment equipment for Maintenance Level I or Maintenance Level II.
7D002	“Source code” for the operation or maintenance…
7D003.a.	“Software” specially designed or modified to…
7D003.b.	“Source code” for…
7D003.c.	Not used
7D003.d.1. to 4. & 7.	Not used
7D004.a. to d. & g.	“Source code” incorporating “development” “technology” specified by…
7D101	“Software” specially designed for the “use” of equipment specified by 7B003 or 7B103 above.
7E001 & 7E002	“Technology” according to the General Technology Note...
7E101	“Technology” according to the General Technology Note for the “use” of equipment specified by 7A117, 7B003, 7B103 and 7D101 above.
Category 8	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
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 specified by 8A001 of this List using navigation data having closed loop servo‑controls and having any of the following: 1. Enabling… 2. Maintaining… 3. Maintaining…
8A002.h.	“Robots” specially designed for underwater use...
8A002.j.	Air independent power systems...
8A002.o.3.	Noise reduction systems for use on vessels...
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 specified by 8A of this List.
8E002.a.	Other “technology”...

Category 9	SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
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 integrated, or designed or modified to be integrated, into a liquid propellant propulsion system, as follows: N.B.: See also 9A119. a. Liquid propellant rocket engines usable in “missiles”, other than those specified by 9A005, having a total impulse capacity equal to or greater than 1.1 MNs; except liquid propellant apogee engines integrated, or designed or modified to be integrated, into a liquid propellant propulsion system, 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	Systems or components, other than those specified by 9A006, usable in “missiles”, as follows, specially designed for liquid rocket propulsion systems: c. Thrust vector control sub‑systems, 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 by 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, other than those specified by 9A008, usable in “missiles” as follows, specially designed for solid rocket propulsion systems: c. Thrust vector control sub‑systems, 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 by 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 non‑weapon payloads: a. Reentry vehicles; b. Heat shields and components therefor fabricated of ceramic or ablative materials; c. Heat sinks and components therefor fabricated of light‑weight, 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 by 9A005 or 9A007.a. above
9B001	Equipment, tooling or fixtures, specially designed for manufacturing gas turbine engine blades, vanes or “tip shrouds”, as follows: a. Directional‑solidification or single‑crystal casting equipment; b. Casting tooling, manufactured from refractory metals or ceramics, as follows: 1. Cores; 2. Shells (moulds); 3. Combined core and shell (mould) units; c. Directional‑solidification…
9B115	Specially designed “production equipment” for the systems, sub‑systems and components specified by 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 by 9A004, or systems, sub‑systems, and components specified by 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”, specified by 9A, 9B or 9E003 of this List.
9D002	“Software” specially designed or modified for the “production” of equipment specified by 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 by 9B116 above.
9E001	“Technology” according to the General Technology Note…
9E002	“Technology” according to the General Technology Note…
9E003.a.1. to 5. and 9E003.a.8.	“Technology” “required” for…
9E003.h.	"Technology" "required" for gas turbine "FADEC systems"…
9E101	“Technology” according to the General Technology Note for the “development” or “production” of goods specified by 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 by 9A004, 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116, 9A119, 9B115, 9B116 or 9D101 above.

Very sensitive list of dual‑use goods and technologies

Note: This List contains Category 0 of the Dual‑Use List and 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 Dual‑Use List for full details. Text that differs from that in the Dual‑Use List is shaded.

Category 0	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
All of Category 0 of Dual‑Use List 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	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
1A002.a.1	“Composite” structures or laminates made from an organic “matrix” and “fibrous or filamentary materials” specified by 1C010.c. or 1C010.d.
1A228	Target assemblies and components for the production of tritium as follows: a. Target assemblies made of or containing lithium enriched in the lithium‑6 isotope specially designed for the production of tritium through irradiation, including insertion in a nuclear reactor; b. Components specially designed for the target assemblies specified by Item 1A228.a. Technical Note: Components specially designed for target assemblies for the production of tritium may include lithium pellets, tritium getters, and specially‑coated cladding.
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 liquid‑liquid 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. c. Ion exchange systems specially designed for lithium isotope separation, and specially designed component parts therefor; d. Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers) specially designed for lithium isotope separation, and specially designed component parts therefor.
1C001	Materials specially designed for absorbing electromagnetic radiation...
1C012	Materials as follows...
1C233	Lithium enriched in the lithium‑6 (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 apply to thermoluminescent dosimeters. Technical Note: The natural isotopic abundance of lithium‑6 is approximately 6.5 weight per cent (7.5 atom per cent).
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 apply to 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 specified by 1A002 or 1C of this List.
1E201	“Technology” according to the General Technology Note for the “use” of goods specified by 1B226, 1B231, 1B233, 1C233 or 1C235.
Category 2	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
None

Category 3	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
3A228	Switching devices, as follows: a. Cold‑cathode 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 spark‑gaps 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. Utilising electrostatic acceleration to induce a tritium‑deuterium nuclear reaction.
3E201	“Technology” according to the General Technology Note for the “use” of equipment specified by 3A228.a., 3A228.b. or 3A231.
Category 4	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
None

Category 5	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
Part 1
5A001.b.5.	Digitally controlled radio receivers...
5A001.h.		Counter Improvised Explosive Device (IED) equipment and related equipment...
5D001.a.	“Software” specially designed for the “development” or “production” of equipment, functions or features specified by 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” specified by Category 5, Part 1 of this List.
Part 2	None

Category 6	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
6A001.a.1.b.1.	Systems or transmitting and receiving arrays, designed for object detection or location, having a sound pressure level exceeding 210 dB (reference 1 μPa at 1 m) and an operating frequency in the band from 30 Hz to 2 kHz.
6A001.a.2.a.1.	Hydrophones...Incorporating…
6A001.a.2.a.2.	Hydrophones...Incorporating flexible assemblies...
6A001.a.2.a.3.	Hydrophones...Having any...
6A001.a.2.a.5.	Hydrophones...Designed to operate …
6A001.a.2.a.6.	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 hydrophone arrays 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.	“Space‑qualified” solid‑state detectors...
6A008.l.3.	Not used
6A203	High‑speed cameras and imaging devices and components therefor, other than those specified by 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 cross‑section…
6D001	“Software” specially designed for the “development” or “production” of equipment specified by 6B008 of this List.
6D003.a.	“Software”, as follows: …
6E001	“Technology” according to the General Technology Note for the “development” of equipment or “software” specified by 6A, 6B, or 6D of this List.
6E002	“Technology” according to the General Technology Note for the “production” of equipment specified by 6A or 6B of this List.
Category 7	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
7D003.a.	“Software” specially designed or modified to…
7D003.b.	“Source code” for…
Category 8	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
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 specified by 8A of this List.
8E001	“Technology” according to the General Technology Note for the “development” or “production” of equipment specified by 8A of this List.
Category 9	VERY SENSITIVE LIST OF DUAL‑USE GOODS AND TECHNOLOGIES
9A011	Ramjet, scramjet or combined cycle engines...
9D001	“Software” specially designed or modified for the “development” of equipment or “technology” specified by 9A or 9E003 of this List.
9D002	“Software” specially designed or modified for the “production” of equipment specified by 9A of this List.
9E001	“Technology” according to the General Technology Note for the “development” of equipment or “software” specified by 9A011 or 9D of this List.
9E002	“Technology” according to the General Technology Note for the “production” of equipment specified by 9A011 of this List.
9E003.a.1.	"Technology" "required" for… Gas turbine blades…
9E003.a.3.a.	"Technology" "required" for… Components... Manufactured from organic "composite" materials designed to operate above 588 K (315°C).

Schedule 1—Repeals

Defence and Strategic Goods List 1996

1 The whole of the instrument

Repeal the instrument.