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Document 32016R1969
Commission Delegated Regulation (EU) 2016/1969 of 12 September 2016 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items
Commission Delegated Regulation (EU) 2016/1969 of 12 September 2016 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items
Commission Delegated Regulation (EU) 2016/1969 of 12 September 2016 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items
C/2016/5707
OJ L 307, 15.11.2016, p. 1–251
(BG, ES, CS, DA, DE, ET, EL, EN, FR, HR, IT, LV, LT, HU, MT, NL, PL, PT, RO, SK, SL, FI, SV)
No longer in force, Date of end of validity: 08/09/2021; Repealed by 32021R0821
15.11.2016 |
EN |
Official Journal of the European Union |
L 307/1 |
COMMISSION DELEGATED REGULATION (EU) 2016/1969
of 12 September 2016
amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items
THE EUROPEAN COMMISSION,
Having regard to the Treaty on the Functioning of the European Union,
Having regard to Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items (1), and in particular Article 15(3) thereof,
Whereas:
(1) |
Regulation (EC) No 428/2009 requires dual-use items to be subject to effective control when they are exported from or transit through the Union, or are delivered to a third country as a result of brokering services provided by a broker resident or established in the Union. |
(2) |
Annex I to Regulation (EC) No 428/2009 establishes the common list of dual-use items that are subject to controls in the Union. Decisions on the items subject to controls are taken within the framework of the Australia Group, the Missile Technology Control Regime, the Nuclear Suppliers Group, the Wassenaar Arrangement and the Chemical Weapons Convention. |
(3) |
The list of dual-use items set out in Annex I to Regulation (EC) No 428/2009 needs to be updated regularly so as to ensure full compliance with international security obligations, to guarantee transparency, and to maintain the competitiveness of economic operators. The changes to the control lists adopted by the international non-proliferation regimes and export control arrangements in 2015 now require another amendment of Annex I to Regulation (EC) No 428/2009. In order to facilitate references for export control authorities and economic operators, Annex I to that Regulation should be updated and consolidated. |
(4) |
Annexes IIa to IIf to Regulation (EC) No 428/2009 establish Union General Export Authorisations. |
(5) |
Annex IIg to Regulation (EC) No 428/2009 establishes a list of dual-use items that shall be excluded from the scope of national general export authorisations and Union General Export Authorisaitons. |
(6) |
Annex IV to Regulation (EC) No 428/2009 establishes authorisation requirements for certain intra-Community transfers. |
(7) |
The amendments to the EU dual-use control list in Annex I necessitate consequential amendments to Annexes IIa to IIg and Annex IV for dual-use items which are also listed in Annexes IIa to IIg and Annex IV. |
(8) |
Regulation (EC) No 428/2009 empowers the Commission to update the list of dual-use items set out in Annex I as well as Annexes IIa to IIg and Annex IV by means of delegated acts, in conformity with the relevant obligations and commitments, and any modifications thereto, that Member States have accepted as members of the international non-proliferation regimes and export control arrangements, or by ratification of relevant international treaties. |
(9) |
Regulation (EC) No 428/2009 should therefore be amended accordingly, |
HAS ADOPTED THIS REGULATION:
Article 1
Annexes I, IIa to IIg and IV to Council Regulation (EC) No 428/2009 are amended in accordance with the Annexes to this Regulation:
(1) |
Annex I is replaced by the text set out in Annex I to this Regulation; |
(2) |
Annexes IIa to IIg are replaced by the text set out in Annex II to this Regulation; |
(3) |
Annex IV is replaced by the text set out in Annex III to this Regulation. |
Article 2
This Regulation shall enter into force on the day following that of its publication in the Official Journal of the European Union.
This Regulation shall be binding in its entirety and directly applicable in all Member States.
Done at Brussels, 12 September 2016.
For the Commission
The President
Jean-Claude JUNCKER
ANNEX I
‘ANNEX I
List referred to in Article 3 of this Regulation
LIST OF DUAL-USE ITEMS
This list implements internationally agreed dual-use controls including the Wassenaar Arrangement, the Missile Technology Control Regime (MTCR), the Nuclear Suppliers' Group (NSG), the Australia Group and the Chemical Weapons Convention (CWC).
CONTENTS
Notes
Acronyms and abbreviations
Definitions
Category 0 |
Nuclear materials, facilities and equipment |
Category 1 |
Special materials and related equipment |
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 |
GENERAL NOTES TO ANNEX I
1. |
For control of goods which are designed or modified for military use, see the relevant list(s) of controls on military goods maintained by individual Member States. References in this Annex that state "SEE ALSO MILITARY GOODS CONTROLS" refer to the same lists. |
2. |
The object of the controls contained in this Annex 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.
|
3. |
Goods specified in this Annex include both new and used goods. |
4. |
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 some forms of the listed chemical have different CAS numbers, and mixtures containing a listed chemical may also have different CAS numbers. |
NUCLEAR TECHNOLOGY NOTE (NTN)
(To be read in conjunction with section E of Category 0.)
The "technology" directly associated with any goods controlled in Category 0 is controlled according to the provisions of Category 0.
"Technology" for the "development", "production" or "use" of goods under control remains under control even when applicable to non-controlled goods.
The approval of goods for export also authorizes the export to the same end-user of the minimum "technology" required for the installation, operation, maintenance and repair of the goods.
Controls on "technology" transfer do not apply to information "in the public domain" or to "basic scientific research".
GENERAL TECHNOLOGY NOTE (GTN)
(To be read in conjunction with section E of Categories 1 to 9.)
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.
"Technology" "required" for the "development", "production" or "use" of goods under control remains under control even when applicable to non-controlled goods.
Controls do not apply to that "technology" which is the minimum necessary for the installation, operation, maintenance (checking) or repair of those goods which are not controlled or whose export has been authorised.
N.B.: |
This does not release such "technology" specified in 1E002.e., 1E002.f., 8E002.a. and 8E002.b. |
Controls on "technology" transfer do not apply to information "in the public domain", to "basic scientific research" or to the minimum necessary information for patent applications.
GENERAL SOFTWARE NOTE (GSN)
(This note overrides any control within section D of Categories 0 to 9.)
Categories 0 to 9 of this list do not control "software" which is any of the following:
a. |
Generally available to the public by being:
|
b. |
"In the public domain"; or |
c. |
The minimum necessary "object code" for the installation, operation, maintenance (checking) or repair of those items whose export has been authorised.
|
GENERAL "INFORMATION SECURITY" NOTE (GISN)
"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.
EDITORIAL PRACTICES IN THE OFFICIAL JOURNAL OF THE EUROPEAN UNION
In accordance with the rules set out in paragraph 6.5 on page 108 of the Interinstitutional style guide (2015 edition), for texts in English published in the Official Journal of the European Union:
— |
a comma is used to separate the whole number from decimals, |
whole numbers are presented in series of three, each series being separated by a thin space. The text reproduced in this annex follows the above-described practice.
ACRONYMS AND ABBREVIATIONS USED IN THIS ANNEX
An acronym or abbreviation, when used as a defined term, will be found in 'Definitions of Terms used in this Annex'.
Acronym or meaning abbreviation |
|
ABEC |
Annular Bearing Engineers Committee |
AGMA |
American Gear Manufacturers' Association |
AHRS |
attitude and heading reference systems |
AISI |
American Iron and Steel Institute |
ALU |
arithmetic logic unit |
ANSI |
American National Standards Institute |
ASTM |
the American Society for Testing and Materials |
ATC |
air traffic control |
AVLIS |
atomic vapour laser isotope separation |
CAD |
computer-aided-design |
CAS |
Chemical Abstracts Service |
CDU |
control and display unit |
CEP |
circular error probable |
CNTD |
controlled nucleation thermal deposition |
CPU |
Central processing unit |
CVD |
chemical vapour deposition |
CW |
chemical warfare |
CW (for lasers) |
continuous wave |
DME |
distance measuring equipment |
DS |
directionally solidified |
EB-PVD |
electron beam physical vapour deposition |
EBU |
European Broadcasting Union |
ECM |
electro-chemical machining |
ECR |
electron cyclotron resonance |
EDM |
electrical discharge machines |
EEPROMS |
electrically erasable programmable read only memory |
EIA |
Electronic Industries Association |
EMC |
electromagnetic compatibility |
ETSI |
European Telecommunications Standards Institute |
FFT |
Fast Fourier Transform |
GLONASS |
global navigation satellite system |
GPS |
global positioning system |
HBT |
hetero-bipolar transistors |
HDDR |
high density digital recording |
HEMT |
high electron mobility transistors |
ICAO |
International Civil Aviation Organisation |
IEC |
International Electro-technical Commission |
IEEE |
Institute of Electrical and Electronic Engineers |
IFOV |
instantaneous-field-of-view |
ILS |
instrument landing system |
IRIG |
inter-range instrumentation group |
ISA |
international standard atmosphere |
ISAR |
inverse synthetic aperture radar |
ISO |
International Organization for Standardization |
ITU |
International Telecommunication Union |
JIS |
Japanese Industrial Standard |
JT |
Joule-Thomson |
LIDAR |
light detection and ranging |
LRU |
line replaceable unit |
MAC |
message authentication code |
Mach |
ratio of speed of an object to speed of sound (after Ernst Mach) |
MLIS |
molecular laser isotopic separation |
MLS |
microwave landing systems |
MOCVD |
metal organic chemical vapour deposition |
MRI |
magnetic resonance imaging |
MTBF |
mean-time-between-failures |
Mtops |
million theoretical operations per second |
MTTF |
mean-time-to-failure |
NBC |
Nuclear, Biological and Chemical |
NDT |
non-destructive test |
PAR |
precision approach radar |
PIN |
personal identification number |
ppm |
parts per million |
PSD |
power spectral density |
QAM |
quadrature-amplitude-modulation |
RF |
radio frequency |
SACMA |
Suppliers of Advanced Composite Materials Association |
SAR |
synthetic aperture radar |
SC |
single crystal |
SLAR |
sidelooking airborne radar |
SMPTE |
Society of Motion Picture and Television Engineers |
SRA |
shop replaceable assembly |
SRAM |
static random access memory |
SRM |
SACMA Recommended Methods |
SSB |
single sideband |
SSR |
secondary surveillance radar |
TCSEC |
trusted computer system evaluation criteria |
TIR |
total indicated reading |
UV |
Ultraviolet |
UTS |
ultimate tensile strength |
VOR |
very high frequency omni-directional range |
YAG |
yttrium/aluminium garnet |
DEFINITIONS OF TERMS USED IN THIS ANNEX
Definitions of terms between 'single quotation marks' are given in a Technical Note to the relevant item.
Definitions of terms between "double quotation marks" are as follows:
N.B.: |
Category references are given in brackets after the defined term. |
"Accuracy" (2 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 8) is a minimum (single) element of the solid state array which has a photoelectric transfer function when exposed to light (electromagnetic) radiation. |
"Adapted for use in war" (1) means any modification or selection (such as altering purity, shelf life, virulence, dissemination characteristics, or resistance to UV radiation) designed to increase the effectiveness in producing casualties in humans or animals, degrading equipment or damaging crops or the environment. |
"Adjusted Peak Performance" (4) is an adjusted peak rate at which "digital computers" perform 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.
|
"Aircraft" (1 7 9) means a fixed wing, swivel wing, rotary wing (helicopter), tilt rotor or tilt-wing airborne vehicle.
|
"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 or measuring errors for the particular coordinate measuring machine 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.
|
"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 |
"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) |
"APP" (4) is equivalent to "Adjusted Peak Performance". |
"Asymmetric algorithm" (5) means a cryptographic algorithm using different, mathematically-related keys for encryption and decryption.
|
"Automatic target tracking" (6) means a processing technique that automatically determines and provides as output an extrapolated value of the most probable position of the target in real time. |
"Average output power" (6) means the total "laser" output energy, in joules, divided by the period over which a series of consecutive pulses is emitted, in seconds. For a series of uniformly spaced pulses it is equal to the total "laser" output energy in a single pulse, in joules, multiplied by the pulse frequency of the "laser", in Hertz. |
"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'.
|
"Basic scientific research" (GTN NTN) means experimental or theoretical work undertaken principally to acquire new knowledge of the fundamental principles of phenomena or observable facts, not primarily directed towards a specific practical aim or objective. |
"Bias" (accelerometer) (7) means the average over a specified time of accelerometer output, measured at specified operating conditions, that has no correlation with input acceleration or rotation. "Bias" is expressed in g or in metres per second squared (g or m/s2). (IEEE Std 528-2001) (Micro g equals 1 × 10– 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). |
"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). |
"Carbon fibre preforms" (1) means an ordered arrangement of uncoated or coated fibres intended to constitute a framework of a part before the "matrix" is introduced to form a "composite". |
"Chemical laser" (6) means a "laser" in which the excited species is produced by the output energy from a chemical reaction. |
"Chemical mixture" (1) means a solid, liquid or gaseous product made up of two or more components which do not react together under the conditions under which the mixture is stored. |
"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. |
"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) means those "aircraft" listed by designation in published airworthiness certification lists by the civil aviation authorities of one or more EU Member States or Wassenaar Arrangement Participating States to fly commercial civil internal and external routes or for legitimate civil, private or business use.
|
"Commingled" (1) means filament to filament blending of thermoplastic fibres and reinforcement fibres in order to produce a fibre reinforcement "matrix" mix in total fibre form. |
"Comminution" (1) means a process to reduce a material to particles by crushing or grinding. |
"Communications channel controller" (4) means the physical interface which controls the flow of synchronous or asynchronous digital information. It is an assembly that can be integrated into computer or telecommunications equipment to provide communications access. |
"Compensation systems" (6) consist of the primary scalar sensor, one or more reference sensors (e.g., vector magnetometers) together with software that permit reduction of rigid body rotation noise of the platform. |
"Composite" (1 2 6 8 9) means a "matrix" and an additional phase or additional phases consisting of particles, whiskers, fibres or any combination thereof, present for a specific purpose or purposes. |
"Compound rotary table" (2) means a table allowing the workpiece to rotate and tilt about two non-parallel axes, which can be coordinated simultaneously for "contouring control". |
"III/V compounds" (3 6) 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). |
"Contouring control" (2) means two or more "numerically controlled" motions operating in accordance with instructions that specify the next required position and the required feed rates to that position. These feed rates are varied in relation to each other so that a desired contour is generated (ref. ISO/DIS 2806 — 1980). |
"Critical temperature" (1 3 5) (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 any of the following:
Technical Notes
|
"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 unauthorized use. "Cryptography" is limited to the transformation of information using one or more 'secret parameters' (e.g., crypto variables) or associated key management.
Technical Note: 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. |
"Deformable mirrors" (6) (also known as adaptive optic mirrors) means mirrors having:
|
"Depleted uranium" (0) means uranium depleted in the isotope 235 below that occurring in nature. |
"Development" (GTN NTN All) is related to all phases 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 joining of at least two separate pieces of 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:
|
"Digital transfer rate" (def) means the total bit rate of the information that is directly transferred on any type of medium.
|
"Direct-acting hydraulic pressing" (2) means a deformation process which uses a fluid-filled flexible bladder in direct contact with the workpiece. |
"Drift rate" (gyro) (7) means the component of gyro output that is functionally independent of input rotation. It is expressed as an angular rate. (IEEE STD 528-2001). |
"Effective gramme" (0 1) of "special fissile material" means:
|
"Electronic assembly" (2 3 4 5) means a number of electronic components (i.e., 'circuit elements', 'discrete components', integrated circuits, etc.) connected together to perform (a) specific function(s), replaceable as an entity and normally capable of being disassembled.
|
"Electronically steerable phased array antenna" (5 6) means an antenna which forms a beam by means of phase coupling, i.e., the beam direction is controlled by the complex excitation coefficients of the radiating elements and the direction of that beam can be varied in azimuth or in elevation, or both, by application, both in transmission and reception, of an electrical signal. |
"Energetic materials" (1) means substances or mixtures that react chemically to release energy required for their intended application. "Explosives", "pyrotechnics" and "propellants" are subclasses of energetic materials. |
"End-effectors" (2) means grippers, 'active tooling units' and any other tooling that is attached to the baseplate on the end of a "robot" manipulator arm.
|
"Equivalent Density" (6) means the mass of an optic per unit optical area projected onto the optical surface. |
"Explosives" (1) means 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. |
"FADEC Systems" (9) means Full Authority Digital Engine Control Systems — A digital electronic control system for a gas turbine engine that is able to autonomously control the engine throughout its whole operating range from demanded engine start until demanded engine shut-down, in both normal and fault conditions. |
"Fibrous or filamentary materials" (0 1 8) include:
|
"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".
|
"Flight control optical sensor array" (7) is a network of distributed optical sensors, using "laser" beams, to provide real-time flight control data for on-board processing. |
"Flight path optimisation" (7) is a procedure that minimizes deviations from a four-dimensional (space and time) desired trajectory based on maximizing performance or effectiveness for mission tasks. |
"Fly-by-light system" (7) means 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) means a 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 8) 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.
|
"Fractional bandwidth" (3 5) means the "instantaneous bandwidth" divided by the centre frequency, expressed as a percentage. |
"Frequency hopping" (5) means a form of "spread spectrum" in which the transmission frequency of a single communication channel is made to change by a random or pseudo-random sequence of discrete steps. |
"Frequency mask trigger" (3) for "signal analysers" is a mechanism where the trigger function is able to select a frequency range to be triggered on as a subset of the acquisition bandwidth while ignoring other signals that may also be present within the same acquisition bandwidth. A "frequency mask trigger" may contain more than one independent set of limits. |
"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:
|
"Frequency synthesiser" (3) means any kind of frequency source, regardless of the actual technique used, providing a multiplicity of simultaneous or alternative output frequencies, from one or more outputs, controlled by, derived from or disciplined by a lesser number of standard (or master) frequencies. |
"Fuel cell" (8) is an electrochemical device that converts chemical energy directly into Direct Current (DC) electricity by consuming fuel from an external source. |
"Fusible" (1) means capable of being cross-linked or polymerized further (cured) by the use of heat, radiation, catalysts, etc., or that can be melted without pyrolysis (charring). |
"Gas Atomisation" (1) means a process to reduce a molten stream of metal alloy to droplets of 500 micrometre diameter or less by a high pressure gas stream. |
"Geographically dispersed" (6) is where each location is distant from any other more than 1 500 m in any direction. Mobile sensors are always considered "geographically dispersed". |
"Guidance set" (7) means systems that integrate the process of measuring and computing a vehicles position and velocity (i.e. navigation) with that of computing and sending commands to the vehicles flight control systems to correct the trajectory. |
"Hot isostatic densification" (2) means the process of pressurising a casting at temperatures exceeding 375 K (102 °C) in a closed cavity through various media (gas, liquid, solid particles, etc.) to create equal force in all directions to reduce or eliminate internal voids in the casting. |
"Hybrid 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:
|
"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), 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 GISN 5) is all the means and functions ensuring the accessibility, confidentiality or integrity of information or communications, excluding the means and functions intended to safeguard against malfunctions. This includes "cryptography", "cryptographic activation", 'cryptanalysis', protection against compromising emanations and computer security. Technical Note: 'Cryptanalysis' : analysis of a cryptographic system or its inputs and outputs to derive confidential variables or sensitive data, including clear text. |
"Instantaneous bandwidth" (3 5 7) means the bandwidth over which output power remains constant within 3 dB without adjustment of other operating parameters. |
"Instrumented range" (6) means the specified unambiguous display range of a radar. |
"Insulation" (9) is applied to the components of a rocket motor, i.e. the case, nozzle, inlets, case closures, and includes cured or 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. |
"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.
|
"Intrusion software" (4) means "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:
Notes:
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 5 6 7 8 9) is an item that produces spatially and temporally coherent light through amplification by stimulated emission of radiation.
|
"Library" (1) (parametric technical database) means a collection of technical information, reference to which may enhance the performance of relevant systems, equipment or components. |
"Lighter-than-air vehicles" (9) means balloons and "airships" that rely on hot air or other lighter-than-air gases such as helium or hydrogen for their lift. |
"Linearity" (2) (usually measured in terms of non-linearity) means the maximum deviation of the actual characteristic (average of upscale and downscale readings), positive or negative, from a straight line so positioned as to equalise and minimise the maximum deviations. |
"Local area network" (4 5) is a data communication system having all of the following characteristics:
|
"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.
|
"Magnetometers" (6) are instruments designed to detect magnetic fields from sources external to the instrument. They consist of a single magnetic field sensing element and associated electronics the output of which is a measure of the magnetic field. |
"Main storage" (4) means the primary storage for data or instructions for rapid access by a central processing unit. It consists of the internal storage of a "digital computer" and any hierarchical extension thereto, such as cache storage or non-sequentially accessed extended storage. |
"Materials resistant to corrosion by UF6" (0) include copper, copper alloys, stainless steel, aluminium, aluminium oxide, aluminium alloys, nickel or alloys containing 60 % or more nickel by weight and fluorinated hydrocarbon polymers. |
"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 (ref. ISO 10360-2). |
"Mechanical Alloying" (1) means an alloying process resulting from the bonding, fracturing and rebonding of elemental and master alloy powders by mechanical impact. Non-metallic particles may be incorporated in the alloy by addition of the appropriate powders. |
"Melt Extraction" (1) means a process to 'solidify rapidly' and extract a ribbon-like alloy product by the insertion of a short segment of a rotating chilled block into a bath of a molten metal alloy.
|
"Melt Spinning" (1) means a process to 'solidify rapidly' a molten metal stream impinging upon a rotating chilled block, forming a flake, ribbon or rod-like product.
|
"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.
|
"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.
|
"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:
|
"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". |
"Multispectral imaging sensors" (6) are capable of simultaneous or serial acquisition of imaging data from two or more discrete spectral bands. Sensors having more than twenty discrete spectral bands are sometimes referred to as hyperspectral imaging sensors. |
"Natural uranium" (0) means uranium containing the mixtures of isotopes occurring in nature. |
"Network access controller" (4) means a physical interface to a distributed switching network. It uses a common medium which operates throughout at the same "digital transfer rate" using arbitration (e.g., token or carrier sense) for transmission. Independently from any other, it selects data packets or data groups (e.g., IEEE 802) addressed to it. It is an assembly that can be integrated into computer or telecommunications equipment to provide communications access. |
"Neural computer" (4) means a computational device designed or modified to mimic the behaviour of a neuron or a collection of neurons, i.e., a computational device which is distinguished by its hardware capability to modulate the weights and numbers of the interconnections of a multiplicity of computational components based on previous data. |
"Nuclear reactor" (0) means a complete reactor capable of operation so as to maintain a controlled self-sustaining fission chain reaction. A "nuclear reactor" includes all the items within or attached directly to the reactor vessel, the equipment which controls the level of power in the core, and the components which normally contain, come into direct contact with or control the primary coolant of the reactor core. |
"Numerical control" (2) means the automatic control of a process performed by a device that makes use of numeric data usually introduced as the operation is in progress (ref. ISO 2382). |
"Object code" (GSN) means an equipment executable form of a convenient expression of one or more processes ("source code" (source language)) which has been compiled by programming system. |
"Operations, Administration or Maintenance" ("OAM") (5) means performing one or more of the following tasks:
|
"Optical computer" (4) means a computer designed or modified to use light to represent data and whose computational logic elements are based on directly coupled optical devices. |
"Optical integrated circuit" (3) means a "monolithic integrated circuit" or a "hybrid integrated circuit", containing one or more parts designed to function as a photosensor or photoemitter or to perform (an) optical or (an) 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.). |
"Participating state" (7 9) is a state participating in the Wassenaar Arrangement (see www.wassenaar.org) |
"Peak power" (6) means the highest power attained in the "pulse duration". |
"Personal area network" (5) means a data communication system having all of the following characteristics:
Technical Note: 'Data device' means equipment capable of transmitting or receiving sequences of digital information. |
"Plasma atomisation" (1) means a process to reduce a molten stream or solid metal to droplets of 500 μm diameter or less, using plasma torches in an inert gas environment. |
"Power management" (7) means changing the transmitted power of the altimeter signal so that received power at the "aircraft" altitude is always at the minimum necessary to determine the altitude. |
"Previously separated" (0 1) means the application of any process intended to increase the concentration of the controlled isotope. |
"Primary flight control" (7) means an "aircraft" stability or manoeuvering control using force/moment generators, i.e., aerodynamic control surfaces or propulsive thrust vectoring. |
"Principal element" (4), as it applies in Category 4, is a "principal element" when its replacement value is more than 35 % of the total value of the system of which it is an element. Element value is the price paid for the element by the manufacturer of the system, or by the system integrator. Total value is the normal international selling price to unrelated parties at the point of manufacture or consolidation of shipment. |
"Production" (GTN NTN All) means all production phases, such as: construction, production engineering, manufacture, integration, assembly (mounting), inspection, testing, quality assurance. |
"Production equipment" (1 7 9) means tooling, templates, jigs, mandrels, moulds, dies, fixtures, alignment mechanisms, test equipment, other machinery and components therefor, limited to those specially designed or modified for "development" or for one or more phases of "production". |
"Production facilities" (7 9) means "production equipment" and specially designed software therefor integrated into installations for "development" or for one or more phases of "production". |
"Programme" (2 6) means a sequence of instructions to carry out a process in, or convertible into, a form executable by an electronic computer. |
"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 and means the time between the half-power points on the leading edge and trailing edge of an individual pulse. |
"Pulsed laser" (6) means a "laser" having a "pulse duration" that is less than or equal to 0,25 seconds. |
"Quantum cryptography" (5) means a family of techniques for the establishment of 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) is Radiant sensitivity (mA/W) = 0,807 × (wavelength in nm) × 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 bandwidth" (3) for "signal analysers" is the widest frequency range for which the analyser can continuously transform time-domain data entirely into frequency-domain results, using a Fourier or other discrete time transformation that processes every incoming time point without gaps or windowing effects that causes a reduction of measured amplitude of more than 3 dB below the actual signal amplitude, while outputting or displaying the transformed data. |
"Real time processing" (2 6 7) means the processing of data by a computer system providing a required level of service, as a function of available resources, within a guaranteed response time, regardless of the load of the system, when stimulated by an external event. |
"Repeatability" (7) means the closeness of agreement among repeated measurements of the same variable under the same operating conditions when changes in conditions or non-operating periods occur between measurements. (Reference: IEEE STD 528-2001 (one sigma standard deviation)) |
"Required" (GTN 1-9), as applied to "technology", refers to only that portion of "technology" which is peculiarly responsible for achieving or extending the controlled performance levels, characteristics or functions. Such "required" "technology" may be shared by different goods. |
"Resolution" (2) means the least increment of a measuring device; on digital instruments, the least significant bit (ref. ANSI B-89.1.12). |
"Riot control agent" (1) means substances which, under the expected conditions of use for riot control purposes, produce rapidly 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) 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:
|
"Rotary atomisation" (1) means a process to reduce a stream or pool of molten metal to droplets to a diameter of 500 micrometre or less by centrifugal force. |
"Roving" (1) is a bundle (typically 12-120) of approximately parallel 'strands'.
|
"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). |
"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. |
"Settling time" (3) means the time required for the output to come within one-half bit of the final value when switching between any two levels of the converter. |
"Signal analysers" (3) means 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 "programmes" or 'microprogrammes' fixed in any tangible medium of expression.
|
"Source code" (or source language) (6 7 9) is a convenient expression of one or more processes which may be turned by a programming system into equipment executable form ("object code" (or object language)). |
"Spacecraft" (7 9) means active and passive satellites and space probes. |
"Spacecraft bus" (9) means equipment that provides the support infrastructure of the "spacecraft" and location for the "spacecraft payload". |
"Spacecraft payload" (9) means equipment, attached to the "spacecraft bus", designed to perform a mission in space (e.g., communications, observation, science). |
"Space-qualified" (3 6 7) means designed, manufactured or qualified through successful testing, for operation at altitudes greater than 100 km above the surface of the Earth.
|
"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) °C) 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) °C) and a relative humidity of (50 ± 5) %. |
"Spinning mass gyros" (7) means gyros which use a continually rotating mass to sense angular motion. |
"Splat Quenching" (1) means a process to 'solidify rapidly' a molten metal stream impinging upon a chilled block, forming a flake-like product.
|
"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. |
"States (not) Party to the Chemical Weapon Convention" (1) are those states for which the Convention on the Prohibition of the Development, Production, Stockpiling and Use of Chemical Weapons has (not) entered into force. (See www.opcw.org) |
"Substrate" (3) means a sheet of base material with or without an interconnection pattern and on which or within which 'discrete components' or integrated circuits or both can be located.
|
"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) means nickel-, cobalt- or iron-base alloys having strengths superior to any alloys in the AISI 300 series at temperatures over 922 K (649 °C) under severe environmental and operating conditions. |
"Superconductive" (1 3 5 6 8) 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.
|
"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.
|
"Systolic array computer" (4) means a computer where the flow and modification of the data is dynamically controllable at the logic gate level by the user. |
"Tape" (1) is a material constructed of interlaced or unidirectional "monofilaments", 'strands', "rovings", "tows", or "yarns", etc., usually pre-impregnated with resin.
|
"Technology" (GTN NTN All) means specific information necessary for the "development", "production" or "use" of goods. This information takes the form of 'technical data' or 'technical assistance'.
|
"Three dimensional integrated circuit" (3) means a collection of semiconductor die, integrated together, and having vias passing completely through at least one die to establish interconnections between die. |
"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). |
"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.
|
"Tow" (1) is a bundle of "monofilaments", usually approximately parallel. |
"Toxins" (1 2) means toxins in the form of deliberately isolated preparations or mixtures, no matter how produced, other than toxins present as contaminants of other materials such as pathological specimens, crops, foodstuffs or seed stocks of "microorganisms". |
"Transfer laser" (6) means a "laser" in which the lasing species is excited through the transfer of energy by collision of a non-lasing atom or molecule with a lasing atom or molecule species. |
"Tunable" (6) means the ability of a "laser" to produce a continuous output at all wavelengths over a range of several "laser" transitions. A line selectable "laser" produces discrete wavelengths within one "laser" transition and is not considered "tunable". |
"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) 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 All) 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 "programmes" by means other than:
|
"Vaccine" (1) is a medicinal product in a pharmaceutical formulation licensed by, or having marketing or clinical trial authorisation from, the regulatory authorities of either the country of manufacture or of use, which is intended to stimulate a protective immunological response in humans or animals in order to prevent disease in those to whom or to which it is administered. |
"Vacuum Atomisation" (1) means a process to reduce a molten stream of metal to droplets of a diameter of 500 micrometre or less by the rapid evolution of a dissolved gas upon exposure to a vacuum. |
"Variable geometry airfoils" (7) means the use of trailing edge flaps or tabs, or leading edge slats or pivoted nose droop, the position of which can be controlled in flight. |
"Yarn" (1) is a bundle of twisted 'strands'.
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CATEGORY 0 — NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT
0A
Systems, Equipment and Components
0A001
"Nuclear reactors" and specially designed or prepared equipment and components therefor, as follows:
a. |
"Nuclear reactors"; |
b. |
Metal vessels, or major shop-fabricated parts therefor, including the reactor vessel head for a reactor pressure vessel, specially designed or prepared to contain the core of a "nuclear reactor"; |
c. |
Manipulative equipment specially designed or prepared for inserting or removing fuel in a "nuclear reactor"; |
d. |
Control rods specially designed or prepared for the control of the fission process in a "nuclear reactor", support or suspension structures therefor, rod drive mechanisms and rod guide tubes; |
e. |
Pressure tubes specially designed or prepared to contain both fuel elements and the primary coolant in a "nuclear reactor"; |
f. |
Zirconium metal tubes or zirconium alloy tubes (or assembles of tubes) specially designed or prepared for use as fuel cladding in a "nuclear reactor", and in quantities exceeding 10 kg;
|
g. |
Coolant pumps or circulators specially designed or prepared for circulating the primary coolant of "nuclear reactors"; |
h. |
'Nuclear reactor internals' specially designed or prepared for use in a "nuclear reactor", including support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates; Technical Note: In 0A001.h. 'nuclear reactor internals' means any major structure within a reactor vessel which has one or more functions such as supporting the core, maintaining fuel alignment, directing primary coolant flow, providing radiation shields for the reactor vessel, and guiding in-core instrumentation. |
i. |
Heat exchangers as follows:
|
j. |
Neutron detectors specially designed or prepared for determining neutron flux levels within the core of a "nuclear reactor"; |
k. |
'External thermal shields' specially designed or prepared for use in a "nuclear reactor" for the reduction of heat loss and also for the containment vessel protection. Technical Note: In 0A001.k. 'external thermal shields' means major structures placed over the reactor vessel which reduce heat loss from the reactor and reduce temperature within the containment vessel. |
0B
Test, Inspection and Production Equipment
0B001
Plant for the separation of isotopes of "natural uranium", "depleted uranium" or"special fissile materials", and specially designed or prepared equipment and components therefor, as follows:
a. |
Plant specially designed for separating isotopes of "natural uranium", "depleted uranium", or "special fissile materials", as follows:
|
b. |
Gas centrifuges and assemblies and components, specially designed or prepared for gas centrifuge separation process, as follows: Technical Note: In 0B001.b. 'high strength-to-density ratio material' means any of the following:
|
c. |
Equipment and components, specially designed or prepared for gaseous diffusion separation process, as follows:
|
d. |
Equipment and components, specially designed or prepared for aerodynamic separation process, as follows:
|
e. |
Equipment and components, specially designed or prepared for chemical exchange separation process, as follows:
|
f. |
Equipment and components, specially designed or prepared for ion-exchange separation process, as follows:
|
g. |
Equipment and components, specially designed or prepared for laser-based separation processes using atomic vapour laser isotope separation, as follows:
|
h. |
Equipment and components, specially designed or prepared for laser-based separation processes using molecular laser isotope separation, as follows:
|
i. |
Equipment and components, specially designed or prepared for plasma separation process, as follows:
|
j. |
Equipment and components, specially designed or prepared for electromagnetic separation process, as follows:
|
0B002
Specially designed or prepared auxiliary systems, equipment and components as follows, for isotope separation plant specified in 0B001, made of or protected by "materials resistant to corrosion by UF6":
a. |
Feed autoclaves, ovens or systems used for passing UF6 to the enrichment process; |
b. |
Desublimers or cold traps, used to remove UF6 from the enrichment process for subsequent transfer upon heating; |
c. |
Product and tails stations for transferring UF6 into containers; |
d. |
Liquefaction or solidification stations used to remove UF6 from the enrichment process by compressing, cooling and converting UF6 to a liquid or solid form; |
e. |
Piping systems and header systems specially designed or prepared for handling UF6 within gaseous diffusion, centrifuge or aerodynamic cascades; |
f. |
Vacuum systems and pumps as follows:
|
g. |
UF6 mass spectrometers/ion sources capable of taking on-line samples from UF6 gas streams and having all of the following:
|
0B003
Plant for the conversion of uranium and equipment specially designed or prepared therefor, as follows:
a. |
Systems for the conversion of uranium ore concentrates to UO3; |
b. |
Systems for the conversion of UO3 to UF6; |
c. |
Systems for the conversion of UO3 to UO2; |
d. |
Systems for the conversion of UO2 to UF4; |
e. |
Systems for the conversion of UF4 to UF6; |
f. |
Systems for the conversion of UF4 to uranium metal; |
g. |
Systems for the conversion of UF6 to UO2; |
h. |
Systems for the conversion of UF6 to UF4; |
i. |
Systems for the conversion of UO2 to UCl4. |
0B004
Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows:
a. |
Plant for the production of heavy water, deuterium or deuterium compounds, as follows:
|
b. |
Equipment and components, as follows:
|
0B005
Plant specially designed for the fabrication of "nuclear reactor" fuel elements and specially designed or prepared equipment therefor.
Technical Note:
Specially designed or prepared equipment for the fabrication of "nuclear reactor" fuel elements includes equipment which:
1. |
Normally comes into direct contact with or directly processes or controls the production flow of nuclear materials; |
2. |
Seals the nuclear materials within the cladding; |
3. |
Checks the integrity of the cladding or the seal; |
4. |
Checks the finish treatment of the sealed fuel; or |
5. |
Is used for assembling reactor elements. |
0B006
Plant for the reprocessing of irradiated "nuclear reactor" fuel elements, and specially designed or prepared equipment and components therefor.
Note: |
0B006 includes:
|
0B007
Plant for the conversion of plutonium and equipment specially designed or prepared therefor, as follows:
a. |
Systems for the conversion of plutonium nitrate to oxide; |
b. |
Systems for plutonium metal production. |
0C
Materials
0C001
"Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing;
Note: |
0C001 does not control the following:
|
0C002
"Special fissile materials"
Note: |
0C002 does not control four "effective grammes" or less when contained in a sensing component in instruments. |
0C003
Deuterium, heavy water (deuterium oxide) and other compounds of deuterium, and mixtures and solutions containing deuterium, in which the isotopic ratio of deuterium to hydrogen exceeds 1:5 000.
0C004
Graphite having a purity level better than 5 parts per million 'boron equivalent' and with a density greater than 1,50 g/cm3 for use in a "nuclear reactor", in quantities exceeding 1 kg.
N.B.: |
SEE ALSO 1C107 |
Note 1: |
For the purpose of export control, the competent authorities of the Member State in which the exporter is established will determine whether or not the exports of graphite meeting the above specifications are for "nuclear reactor" use. |
Note 2: |
In 0C004, 'boron equivalent' (BE) is defined as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:
|
0C005
Specially prepared compounds or powders for the manufacture of gaseous diffusion barriers, resistant to corrosion by UF6 (e.g. nickel or alloy containing 60 weight per cent or more nickel, aluminium oxide and fully fluorinated hydrocarbon polymers), having a purity of 99,9 % by weight or more and a particle size less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard and a high degree of particle size uniformity.
0D
Software
0D001
"Software" specially designed or modified for the "development", "production" or "use" of goods specified in this Category.
0E
Technology
0E001
"Technology" according to the Nuclear Technology Note for the "development", "production" or "use" of goods specified in this Category.
CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT
1A
Systems, Equipment and Components
1A001
Components made from fluorinated compounds, as follows:
a. |
Seals, gaskets, sealants or fuel bladders, specially designed for "aircraft" or aerospace use, made from more than 50 % by weight of any of the materials specified in 1C009.b. or 1C009.c.; |
b. |
Not used; |
c. |
Not used. |
1A002
"Composite" structures or laminates, having any of the following:
N.B: |
SEE ALSO 1A202, 9A010 and 9A110 |
a. |
Consisting of an organic "matrix" and materials specified in 1C010.c., 1C010.d. or 1C010.e.; or |
b. |
Consisting of a metal or carbon "matrix", and any of the following:
|
Note 1: |
1A002 does not control "composite" structures or laminates made from epoxy resin impregnated carbon "fibrous or filamentary materials" for the repair of "civil aircraft" structures or laminates, having all of the following:
|
Note 2: |
1A002 does not control semi-finished items, specially designed for purely civilian applications as follows:
|
Note 3: |
1A002.b.1. does not control semi-finished items containing a maximum of two dimensions of interwoven filaments and specially designed for applications as follows:
|
Note 4: |
1A002 does not control finished items specially designed for a specific application. |
1A003
Manufactures of non-"fusible" aromatic polyimides in film, sheet, tape or ribbon form having any of the following:
a. |
A thickness exceeding 0,254 mm; or |
b. |
Coated or laminated with carbon, graphite, metals or magnetic substances. |
Note: |
1A003 does not control manufactures when coated or laminated with copper and designed for the production of electronic printed circuit boards. |
N.B.: |
For "fusible" aromatic polyimides in any form, see 1C008.a.3. |
1A004
Protective and detection equipment and components not specially designed for military use, as follows:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS, 2B351 AND 2B352. |
a. |
Full face masks, filter canisters and decontamination equipment therefor, designed or modified for defence against any of the following, and specially designed components therefor:
Technical Note: For the purposes of 1A004.a.:
|
b. |
Protective suits, gloves and shoes, specially designed or modified for defence against any of the following:
|
c. |
Detection systems, specially designed or modified for detection or identification of any of the following, and specially designed components therefor:
|
d. |
Electronic equipment designed for automatically detecting or identifying the presence of "explosives" residues and utilising 'trace detection' techniques (e.g., surface acoustic wave, ion mobility spectrometry, differential mobility spectrometry, mass spectrometry). Technical Note: 'Trace detection' is defined as the capability to detect less than 1 ppm vapour, or 1 mg solid or liquid.
Technical Notes:
|
1A005
Body armour and components therefor, as follows:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS. |
a. |
Soft body armour not manufactured to military standards or specifications, or to their equivalents, and specially designed components therefor; |
b. |
Hard body armour plates providing ballistic protection equal to or less than level IIIA (NIJ 0101.06, July 2008) or national equivalents. |
N.B.: |
For "fibrous or filamentary materials" used in the manufacture of body armour, see 1C010. |
Note 1: |
1A005 does not control body armour when accompanying its user for the user's own personal protection. |
Note 2: |
1A005 does not control body armour designed to provide frontal protection only from both fragment and blast from non-military explosive devices. |
Note 3: |
1A005 does not control body armour designed to provide protection only from knife, spike, needle or blunt trauma. |
1A006
Equipment, specially designed or modified for the disposal of improvised explosive devices, as follows, and specially designed components and accessories therefor:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS. |
a. |
Remotely operated vehicles; |
b. |
'Disruptors'. |
Technical Note:
'Disruptors' are devices specially designed for the purpose of preventing the operation of an explosive device by projecting a liquid, solid or frangible projectile.
Note: |
1A006 does not control equipment when accompanying its operator. |
1A007
Equipment and devices, specially designed to initiate charges and devices containing "energetic materials", by electrical means, as follows:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS, 3A229 AND 3A232. |
a. |
Explosive detonator firing sets designed to drive explosive detonators specified in 1A007.b.; |
b. |
Electrically driven explosive detonators as follows:
|
Technical Notes:
1. |
The word initiator or igniter is sometimes used in place of the word detonator. |
2. |
For the purpose of 1A007.b. the detonators of concern all utilise a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporises when a fast, high-current electrical pulse is passed through it. In non-slapper types, the exploding conductor starts a chemical detonation in a contacting high explosive material such as PETN (pentaerythritoltetranitrate). In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. |
1A008
Charges, devices and components, as follows:
a. |
'Shaped charges' having all of the following:
|
b. |
Linear shaped cutting charges having all of the following, and specially designed components therefor:
|
c. |
Detonating cord with explosive core load greater than 64 g/m; |
d. |
Cutters, other than those specified in 1A008.b., and severing tools, having a Net Explosive Quantity (NEQ) greater than 3,5 kg. |
Technical Note:
'Shaped charges' are explosive charges shaped to focus the effects of the explosive blast.
1A102
Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
1A202
Composite structures, other than those specified in 1A002, in the form of tubes and having both of the following characteristics:
N.B.:
SEE ALSO 9A010 AND 9A110.
a. |
An inside diameter of between 75 mm and 400 mm; and |
b. |
Made with any of the "fibrous or filamentary materials" specified in 1C010.a. or b. or 1C210.a. or with carbon prepreg materials specified in 1C210.c. |
1A225
Platinized catalysts specially designed or prepared for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.
1A226
Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics:
a. |
Made of phosphor bronze mesh chemically treated to improve wettability; and |
b. |
Designed to be used in vacuum distillation towers. |
1A227
High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor:
a. |
A 'cold area' greater than 0,09 m2; |
b. |
A density greater than 3 g/cm3; and |
c. |
A thickness of 100 mm or greater. |
Technical Note:
In 1A227 the term 'cold area' means the viewing area of the window exposed to the lowest level of radiation in the design application.
1B
Test, Inspection and Production Equipment
1B001
Equipment for the production or inspection of "composite" structures or laminates specified in 1A002 or "fibrous or filamentary materials" specified in 1C010, as follows, and specially designed components and accessories therefor:
N.B.: |
SEE ALSO 1B101 AND 1B201. |
a. |
Filament winding machines, of which the motions for positioning, wrapping and winding fibres are coordinated and programmed in three or more 'primary servo positioning' axes, specially designed for the manufacture of "composite" structures or laminates, from "fibrous or filamentary materials"; |
b. |
'Tape-laying machines', of which the motions for positioning and laying tape are coordinated and programmed in five or more 'primary servo positioning' axes, specially designed for the manufacture of "composite" airframe or 'missile' structures;
Technical Note: For the purposes of 1B001.b., 'tape-laying machines' have the ability to lay one or more 'filament bands' limited to widths greater than 25 mm and less than or equal to 305 mm, and to cut and restart individual 'filament band' courses during the laying process. |
c. |
Multidirectional, multidimensional weaving machines or interlacing machines, including adapters and modification kits, specially designed or modified for weaving, interlacing or braiding fibres, for "composite" structures; Technical Note: For the purposes of 1B001.c., the technique of interlacing includes knitting. |
d. |
Equipment specially designed or adapted for the production of reinforcement fibres, as follows:
|
e. |
Equipment for producing prepregs specified in 1C010.e. by the hot melt method; |
f. |
Non-destructive inspection equipment specially designed for "composite" materials, as follows:
|
g. |
'Tow-placement machines', of which the motions for positioning and laying tows are coordinated and programmed in two or more 'primary servo positioning' axes, specially designed for the manufacture of "composite" airframe or 'missile' structures. Technical Note: For the purposes of 1B001.g., 'tow-placement machines' have the ability to place one or more 'filament bands' having widths less than or equal to 25 mm, and to cut and restart individual 'filament band' courses during the placement process. |
Technical Note:
1. |
For the purpose of 1B001, 'primary servo positioning' axes control, under computer program direction, the position of the end effector (i.e., head) in space relative to the work piece at the correct orientation and direction to achieve the desired process. |
2. |
For the purposes of 1B001., a 'filament band' is a single continuous width of fully or partially resin-impregnated tape, tow or fibre. |
1B002
Equipment for producing metal alloys, metal alloy powder or alloyed materials, specially designed to avoid contamination and specially designed for use in one of the processes specified in 1C002.c.2.
N.B.: |
SEE ALSO 1B102. |
1B003
Tools, dies, moulds or fixtures, for "superplastic forming" or "diffusion bonding" titanium, aluminium or their alloys, specially designed for the manufacture of any of the following:
a. |
Airframe or aerospace structures; |
b. |
"Aircraft" or aerospace engines; or |
c. |
Specially designed components for structures specified in 1B003.a. or for engines specified in 1B003.b. |
1B101
Equipment, other than that specified in 1B001, for the "production" of structural composites as follows; and specially designed components and accessories therefor:
N.B.: |
SEE ALSO 1B201. |
Note: |
Components and accessories specified in 1B101 include moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof. |
a. |
Filament winding machines or fibre placement machines, of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and coordinating and programming controls; |
b. |
Tape-laying machines of which the motions for positioning and laying tape and sheets can be coordinated and programmed in two or more axes, designed for the manufacture of composite airframe and "missile" structures; |
c. |
Equipment designed or modified for the "production" of "fibrous or filamentary materials" as follows:
|
d. |
Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry 9C110.
|
1B102
Metal powder "production equipment", other than that specified in 1B002, and components as follows:
N.B.: |
SEE ALSO 1B115.b. |
a. |
Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical, spheroidal or atomised materials specified in 1C011.a., 1C011.b., 1C111.a.1., 1C111.a.2. or in the Military Goods Controls. |
b. |
Specially designed components for "production equipment" specified in 1B002 or 1B102.a. |
Note: |
1B102 includes:
|
1B115
Equipment, other than that specified in 1B002 or 1B102, for the production of propellant and propellant constituents, as follows, and specially designed components therefor:
a. |
"Production equipment" for the "production", handling or acceptance testing of liquid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls; |
b. |
"Production equipment" for the "production", handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls.
|
Note 1: |
For equipment specially designed for the production of military goods, see the Military Goods Controls. |
Note 2: |
1B115 does not control equipment for the "production", handling and acceptance testing of boron carbide. |
1B116
Specially designed nozzles for producing pyrolitically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa.
1B117
Batch mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with temperature control capability of the mixing chamber and having all of the following, and specially designed components therefor:
a. |
A total volumetric capacity of 110 litres or more; and |
b. |
At least one 'mixing/kneading shaft' mounted off centre. |
Note: |
In 1B117.b. the term 'mixing/kneading shaft' does not refer to deagglomerators or knife-spindles. |
1B118
Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor:
a. |
Two or more mixing/kneading shafts; or |
b. |
A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber. |
1B119
Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls, and specially designed components therefor.
1B201
Filament winding machines, other than those specified in 1B001 or 1B101, and related equipment, as follows:
a. |
Filament winding machines having all of the following characteristics:
|
b. |
Coordinating and programming controls for the filament winding machines specified in 1B201.a.; |
c. |
Precision mandrels for the filament winding machines specified in 1B201.a. |
1B225
Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.
1B226
Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.
Note: |
1B226 includes separators:
|
1B228
Hydrogen-cryogenic distillation columns having all of the following characteristics:
a. |
Designed for operation with internal temperatures of 35 K (– 238 °C) or less; |
b. |
Designed for operation at an internal pressure of 0,5 to 5 MPa; |
c. |
Constructed of either:
|
d. |
With internal diameters of 30 cm or greater and 'effective lengths' of 4 m or greater. |
Technical Note:
In 1B228 'effective length' means the active height of packing material in a packed-type column, or the active height of internal contactor plates in a plate-type column.
1B229
Water-hydrogen sulphide exchange tray columns and 'internal contactors', as follows:
N.B.: |
For columns which are specially designed or prepared for the production of heavy water see 0B004. |
a. |
Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:
|
b. |
'Internal contactors' for the water-hydrogen sulphide exchange tray columns specified in 1B229.a. |
Technical Note:
'Internal contactors' of the columns are segmented trays which have an effective assembled diameter of 1,8 m or greater, are designed to facilitate countercurrent contacting and are constructed of stainless steels with a carbon content of 0,03 % or less. These may be sieve trays, valve trays, bubble cap trays, or turbogrid trays.
1B230
Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:
a. |
Airtight (i.e., hermetically sealed); |
b. |
A capacity greater than 8,5 m3/h; and |
c. |
Either of the following characteristics:
|
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:
|
1B232
Turboexpanders or turboexpander-compressor sets having both of the following characteristics:
a. |
Designed for operation with an outlet temperature of 35 K (– 238 °C) or less; and |
b. |
Designed for a throughput of hydrogen gas of 1 000 kg/h or greater. |
1B233
Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows:
a. |
Facilities or plants for the separation of lithium isotopes; |
b. |
Equipment for the separation of lithium isotopes based on the lithium-mercury amalgam process, as follows:
|
c. |
Ion exchange systems specially designed for lithium isotope separation, and specially designed components therefor; |
d. |
Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers), specially designed for lithium isotope separation, and specially designed components therefor. |
1B234
High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS. |
a. |
Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; and |
b. |
Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information. |
1C
Materials
Technical Note:
Metals and alloys:
Unless provision to the contrary is made, the words 'metals' and 'alloys' in 1C001 to 1C012 cover crude and semi-fabricated forms, as follows:
Crude forms: Anodes, balls, bars (including notched bars and wire bars), billets, blocks, blooms, brickets, cakes, cathodes, crystals, cubes, dice, grains, granules, ingots, lumps, pellets, pigs, powder, rondelles, shot, slabs, slugs, sponge, sticks; |
Semi-fabricated forms (whether or not coated, plated, drilled or punched):
|
The object of the control should not be defeated by the export of non-listed forms alleged to be finished products but representing in reality crude forms or semi-fabricated forms.
1C001
Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows:
N.B. |
SEE ALSO 1C101. |
a. |
Materials for absorbing frequencies exceeding 2 × 108 Hz but less than 3 × 1012 Hz;
|
b. |
Materials for absorbing frequencies exceeding 1,5 × 1014 Hz but less than 3,7 × 1014 Hz and not transparent to visible light;
|
c. |
Intrinsically conductive polymeric materials with a 'bulk electrical conductivity' exceeding 10 000 S/m (Siemens per metre) or a 'sheet (surface) resistivity' of less than 100 ohms/square, based on any of the following polymers:
Technical Note: 'Bulk electrical conductivity' and 'sheet (surface) resistivity' should be determined using ASTM D-257 or national equivalents. |
1C002
Metal alloys, metal alloy powder and alloyed materials, as follows:
N.B.: |
SEE ALSO 1C202. |
Note: |
1C002 does not control metal alloys, metal alloy powder and alloyed materials, specially formulated for coating purposes. |
Technical Notes:
1. |
The metal alloys in 1C002 are those containing a higher percentage by weight of the stated metal than of any other element. |
2. |
'Stress-rupture life' should be measured in accordance with ASTM standard E-139 or national equivalents. |
3. |
'Low cycle fatigue life' should be measured in accordance with ASTM Standard E-606 'Recommended Practice for Constant-Amplitude Low-Cycle Fatigue Testing' or national equivalents. Testing should be axial with an average stress ratio equal to 1 and a stress-concentration factor (Kt) equal to 1. The average stress is defined as maximum stress minus minimum stress divided by maximum stress. |
a. |
Aluminides, as follows:
|
b. |
Metal alloys, as follows, made from the powder or particulate material specified in 1C002.c.:
|
c. |
Metal alloy powder or particulate material, having all of the following:
|
d. |
Alloyed materials having all of the following:
|
1C003
Magnetic metals, of all types and of whatever form, having any of the following:
a. |
Initial relative permeability of 120 000 or more and a thickness of 0,05 mm or less; Technical Note: Measurement of initial relative permeability must be performed on fully annealed materials. |
b. |
Magnetostrictive alloys having any of the following:
|
c. |
Amorphous or 'nanocrystalline' alloy strips, having all of the following:
Technical Note: 'Nanocrystalline' materials in 1C003.c. are those materials having a crystal grain size of 50 nm or less, as determined by X-ray diffraction. |
1C004
Uranium titanium alloys or tungsten alloys with a "matrix" based on iron, nickel or copper, having all of the following:
a. |
A density exceeding 17,5 g/cm3; |
b. |
An elastic limit exceeding 880 MPa; |
c. |
An ultimate tensile strength exceeding 1 270 MPa; and |
d. |
An elongation exceeding 8 %. |
1C005
"Superconductive" "composite" conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows:
a. |
"Superconductive" "composite" conductors containing one or more niobium-titanium 'filaments', having all of the following:
|
b. |
"Superconductive" "composite" conductors consisting of one or more "superconductive" 'filaments' other than niobium-titanium, having all of the following:
|
c. |
"Superconductive" "composite" conductors consisting of one or more "superconductive" 'filaments' which remain "superconductive" above 115 K (– 158,16 °C). |
Technical Note:
For the purpose of 1C005 'filaments' may be in wire, cylinder, film, tape or ribbon form.
1C006
Fluids and lubricating materials, as follows:
a. |
Not used; |
b. |
Lubricating materials containing, as their principal ingredients, any of the following:
|
c. |
Damping or flotation fluids having all of the following:
|
d. |
Fluorocarbon electronic cooling fluids having all of the following:
|
1C007
Ceramic powders, non-"composite" ceramic materials, ceramic-"matrix" "composite" materials and precursor materials, as follows:
N.B.: |
SEE ALSO 1C107. |
a. |
Ceramic powders of single or complex borides of titanium, having total metallic impurities, excluding intentional additions, of less than 5 000 ppm, an average particle size equal to or less than 5 μm and no more than 10 % of the particles larger than 10 μm; |
b. |
Non-"composite" ceramic materials in crude or semi-fabricated form, composed of borides of titanium with a density of 98 % or more of the theoretical density;
|
c. |
Ceramic-ceramic "composite" materials with a glass or oxide-"matrix" and reinforced with fibres having all of the following:
|
d. |
Ceramic-ceramic "composite" materials, with or without a continuous metallic phase, incorporating particles, whiskers or fibres, where carbides or nitrides of silicon, zirconium or boron form the "matrix"; |
e. |
Precursor materials (i.e., special purpose polymeric or metallo-organic materials) for producing any phase or phases of the materials specified in 1C007.c., as follows:
|
f. |
Ceramic-ceramic "composite" materials with an oxide or glass "matrix" reinforced with continuous fibres from any of the following systems:
|
1C008
Non-fluorinated polymeric substances as follows:
a. |
Imides, as follows:
|
b. |
Not used; |
c. |
Not used; |
d. |
Polyarylene ketones; |
e. |
Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof; |
f. |
Polybiphenylenethersulphone having a 'glass transition temperature (Tg)' exceeding 563 K (290 °C). |
Technical Note:
1. |
The 'glass transition temperature (Tg)' for 1C008.a.2. thermoplastic materials, 1C008.a.4. materials and 1C008.f materials is determined using the method described in ISO 11357-2 (1999) or national equivalents |
2. |
The 'glass transition temperature (Tg)' for 1C008.a.2. thermosetting materials and 1C008.a.3. materials is determined using the 3-point bend method described in ASTM D 7028-07 or equivalent national standard. The test is to be performed using a dry test specimen which has attained a minimum of 90 % degree of cure as specified by ASTM E 2160-04 or equivalent national standard, and was cured using the combination of standard- and post-cure processes that yield the highest Tg. |
1C009
Unprocessed fluorinated compounds as follows:
a. |
Not used; |
b. |
Fluorinated polyimides containing 10 % by weight or more of combined fluorine; |
c. |
Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine. |
1C010
"Fibrous or filamentary materials", as follows:
N.B.: |
SEE ALSO 1C210 AND 9C110. |
Technical Notes:
1. |
For the purpose of calculating "specific tensile strength", "specific modulus" or specific weight of "fibrous or filamentary materials" in 1C010.a., 1C010.b., 1C010.c. or 1C010.e.1.b., the tensile strength and modulus should be determined by using Method A described in ISO 10618 (2004) or national equivalents. |
2. |
Assessing the "specific tensile strength", "specific modulus" or specific weight of non-unidirectional "fibrous or filamentary materials" (e.g., fabrics, random mats or braids) in 1C010 is to be based on the mechanical properties of the constituent unidirectional monofilaments (e.g., monofilaments, yarns, rovings or tows) prior to processing into the non-unidirectional "fibrous or filamentary materials". |
a. |
Organic "fibrous or filamentary materials", having all of the following:
|
b. |
Carbon "fibrous or filamentary materials", having all of the following:
|
c. |
Inorganic "fibrous or filamentary materials", having all of the following:
|
d. |
"Fibrous or filamentary materials", having any of the following:
|
e. |
Fully or partially resin-impregnated or pitch-impregnated "fibrous or filamentary materials" (prepregs), metal or carbon-coated "fibrous or filamentary materials" (preforms) or "carbon fibre preforms", having all of the following:
Technical Note: The 'Dynamic Mechanical Analysis glass transition temperature (DMA Tg)' for materials specified by 1C010.e. is determined using the method described in ASTM D 7028-07, or equivalent national standard, on a dry test specimen. In the case of thermoset materials, degree of cure of a dry test specimen shall be a minimum of 90 % as defined by ASTM E 2160-04 or equivalent national standard. |
1C011
Metals and compounds, as follows:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS and 1C111. |
a. |
Metals in particle sizes of less than 60 μm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys thereof; Technical Note: The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.
|
b. |
Boron or boron alloys, with a particle size of 60 μm or less, as follows:
|
c. |
Guanidine nitrate (CAS 506-93-4); |
d. |
Nitroguanidine (NQ) (CAS 556-88-7). |
N.B.: |
See also Military Goods Controls for metal powders mixed with other substances to form a mixture formulated for military purposes. |
1C012
Materials as follows:
Technical Note:
These materials are typically used for nuclear heat sources.
a. |
Plutonium in any form with a plutonium isotopic assay of plutonium-238 of more than 50 % by weight;
|
b. |
"Previously separated" neptunium-237 in any form.
|
1C101
Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in 'missiles', "missile" subsystems or unmanned aerial vehicles specified in 9A012 or 9A112.a.
Note 1: |
1C101 includes:
|
Note 2: |
1C101 does not include coatings when specially used for the thermal control of satellites. |
Technical Note:
In 1C101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
1C102
Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
1C107
Graphite and ceramic materials, other than those specified in 1C007, as follows:
a. |
Fine grain graphites with a bulk density of 1,72 g/cm3 or greater, measured at 288 K (15 °C), and having a grain size of 100 μm or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:
|
b. |
Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
|
c. |
Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in radomes usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; |
d. |
Bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; |
e. |
Reinforced silicon-carbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
1C111
Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:
a. |
Propulsive substances:
|
b. |
Polymeric substances:
|
c. |
Other propellant additives and agents:
|
Note: |
For propellants and constituent chemicals for propellants not specified in 1C111, see the Military Goods Controls. |
1C116
Maraging steels, useable in 'missiles', having all of the following:
N.B.: |
SEE ALSO 1C216. |
a. |
Having an ultimate tensile strength, measured at 293 K (20 °C), equal to or greater than:
|
b. |
Any of the following forms:
|
Technical Note 1:
Maraging steels are iron alloy:
1. |
Generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and age-hardening of the alloy; and |
2. |
Subjected to heat treatment cycles to facilitate the martensitic transformation process (solution annealed stage) and subsequently age hardened (precipitation hardened stage). |
Technical Note 2:
In 1C116 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
1C117
Materials for the fabrication of 'missiles' components as follows:
a. |
Tungsten and alloys in particulate form with a tungsten content of 97 % by weight or more and a particle size of 50 × 10– 6 m (50 μm) or less; |
b. |
Molybdenum and alloys in particulate form with a molybdenum content of 97 % by weight or more and a particle size of 50 × 10– 6 m (50 μm) or less; |
c. |
Tungsten materials in solid form having all of the following:
|
Technical Note:
In 1C117 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
1C118
Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:
a. |
Having all of the following characteristics:
|
b. |
Having any of the following forms:
|
1C202
Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:
a. |
Aluminium alloys having both of the following characteristics:
|
b. |
Titanium alloys having both of the following characteristics:
|
Technical Note:
The phrase alloys 'capable of' encompasses alloys before or after heat treatment.
1C210
'Fibrous or filamentary materials' or prepregs, other than those specified in 1C010.a., b. or e., as follows:
a. |
Carbon or aramid 'fibrous or filamentary materials' having either of the following characteristics:
|
b. |
Glass 'fibrous or filamentary materials' having both of the following characteristics:
|
c. |
Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass 'fibrous or filamentary materials' specified in 1C210.a. or b. Technical Note: The resin forms the matrix of the composite. |
Note: |
In 1C210, 'fibrous or filamentary materials' is restricted to continuous "monofilaments", "yarns", "rovings", "tows" or "tapes". |
1C216
Maraging steel, other than that specified in 1C116, 'capable of' an ultimate tensile strength of 1 950 MPa or more, at 293 K (20 °C).
Note: |
1C216 does not control forms in which all linear dimensions are 75 mm or less. |
Technical Note:
The phrase maraging steel 'capable of' encompasses maraging steel before or after heat treatment.
1C225
Boron enriched in the boron-10 (10B) isotope to greater than its natural isotopic abundance, as follows: elemental boron, compounds, mixtures containing boron, manufactures thereof, waste or scrap of any of the foregoing.
Note: |
In 1C225 mixtures containing boron include boron loaded materials. |
Technical Note:
The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent).
1C226
Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, other than that specified by 1C117, having both of the following characteristics:
a. |
In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; and |
b. |
A mass greater than 20 kg. |
Note: |
1C226 does not control manufactures specially designed as weights or gamma-ray collimators. |
1C227
Calcium having both of the following characteristics:
a. |
Containing less than 1 000 parts per million by weight of metallic impurities other than magnesium; and |
b. |
Containing less than 10 parts per million by weight of boron. |
1C228
Magnesium having both of the following characteristics:
a. |
Containing less than 200 parts per million by weight of metallic impurities other than calcium; and |
b. |
Containing less than 10 parts per million by weight of boron. |
1C229
Bismuth having both of the following characteristics:
a. |
A purity of 99,99 % or greater by weight; and |
b. |
Containing less than 10 ppm (parts per million) by weight of silver. |
1C230
Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing, other than that specified in the Military Goods Controls.
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS. |
Note: |
1C230 does not control the following:
|
1C231
Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.
1C232
Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.
Note: |
1C232 does not control a product or device containing less than 1 g of helium-3. |
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 control thermoluminescent dosimeters. |
Technical Note:
The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7,5 atom per cent).
1C234
Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing, other than those specified in 0A001.f.
Note: |
1C234 does not control zirconium in the form of foil having a thickness of 0,10 mm or less. |
1C235
Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000, and products or devices containing any of the foregoing.
Note: |
1C235 does not control a product or device containing less than 1,48 × 103 GBq (40 Ci) of tritium. |
1C236
'Radionuclides' appropriate for making neutron sources based on alpha-n reaction, other than those specified in 0C001 and 1C012.a., in the following forms:
a. |
Elemental; |
b. |
Compounds having a total activity of 37 GBq/kg (1 Ci/kg) or greater; |
c. |
Mixtures having a total activity of 37 GBq/kg (1 Ci/kg) or greater; |
d. |
Products or devices containing any of the foregoing. |
Note: |
1C236 does not control a product or device containing less than 3,7 GBq (100 millicuries) of activity. |
Technical Note:
In 1C236 'radionuclides' are any of the following:
— |
Actinium-225 (Ac-225) |
— |
Actinium-227 (Ac-227) |
— |
Californium-253 (Cf-253) |
— |
Curium-240 (Cm-240) |
— |
Curium-241 (Cm-241) |
— |
Curium-242 (Cm-242) |
— |
Curium-243 (Cm-243) |
— |
Curium-244 (Cm-244) |
— |
Einsteinium-253 (Es-253) |
— |
Einsteinium-254 (Es-254) |
— |
Gadolinium-148 (Gd-148) |
— |
Plutonium-236 (Pu-236) |
— |
Plutonium-238 (Pu-238) |
— |
Polonium-208 (Po-208) |
— |
Polonium-209 (Po-209) |
— |
Polonium-210 (Po-210) |
— |
Radium-223 (Ra-223) |
— |
Thorium-227 (Th-227) |
— |
Thorium-228 (Th-228) |
— |
Uranium-230 (U-230) |
— |
Uranium-232 (U-232) |
1C237
Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures thereof, and products or devices containing any of the foregoing.
Note: |
1C237 does not control the following:
|
1C238
Chlorine trifluoride (ClF3).
1C239
High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8 000 m/s.
1C240
Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:
a. |
Nickel powder having both of the following characteristics:
|
b. |
Porous nickel metal produced from materials specified in 1C240.a. |
Note: |
1C240 does not control the following:
|
Technical Note:
1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure.
1C241
Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics:
a. |
In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and |
b. |
A mass greater than 20kg. |
1C350
Chemicals, which may be used as precursors for toxic chemical agents, as follows, and "chemical mixtures" containing one or more thereof:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS AND 1C450. |
1. |
Thiodiglycol (111-48-8); |
2. |
Phosphorus oxychloride (10025-87-3); |
3. |
Dimethyl methylphosphonate (756-79-6); |
4. |
SEE MILITARY GOODS CONTROLS for Methyl phosphonyl difluoride (676-99-3); |
5. |
Methyl phosphonyl dichloride (676-97-1); |
6. |
Dimethyl phosphite (DMP) (868-85-9); |
7. |
Phosphorus trichloride (7719-12-2); |
8. |
Trimethyl phosphite (TMP) (121-45-9); |
9. |
Thionyl chloride (7719-09-7); |
10. |
3-Hydroxy-1-methylpiperidine (3554-74-3); |
11. |
N,N-Diisopropyl-(beta)-aminoethyl chloride (96-79-7); |
12. |
N,N-Diisopropyl-(beta)-aminoethane thiol (5842-07-9); |
13. |
3-Quinuclidinol (1619-34-7); |
14. |
Potassium fluoride (7789-23-3); |
15. |
2-Chloroethanol (107-07-3); |
16. |
Dimethylamine (124-40-3); |
17. |
Diethyl ethylphosphonate (78-38-6); |
18. |
Diethyl N,N-dimethylphosphoramidate (2404-03-7); |
19. |
Diethyl phosphite (762-04-9); |
20. |
Dimethylamine hydrochloride (506-59-2); |
21. |
Ethyl phosphinyl dichloride (1498-40-4); |
22. |
Ethyl phosphonyl dichloride (1066-50-8); |
23. |
SEE MILITARY GOODS CONTROLS for Ethyl phosphonyl difluoride (753-98-0); |
24. |
Hydrogen fluoride (7664-39-3); |
25. |
Methyl benzilate (76-89-1); |
26. |
Methyl phosphinyl dichloride (676-83-5); |
27. |
N,N-Diisopropyl-(beta)-amino ethanol (96-80-0); |
28. |
Pinacolyl alcohol (464-07-3); |
29. |
SEE MILITARY GOODS CONTROLS for O-Ethyl O-2-diisopropylaminoethyl methylphosphonite (QL) (57856-11-8); |
30. |
Triethyl phosphite (122-52-1); |
31. |
Arsenic trichloride (7784-34-1); |
32. |
Benzilic acid (76-93-7); |
33. |
Diethyl methylphosphonite (15715-41-0); |
34. |
Dimethyl ethylphosphonate (6163-75-3); |
35. |
Ethyl phosphinyl difluoride (430-78-4); |
36. |
Methyl phosphinyl difluoride (753-59-3); |
37. |
3-Quinuclidone (3731-38-2); |
38. |
Phosphorus pentachloride (10026-13-8); |
39. |
Pinacolone (75-97-8); |
40. |
Potassium cyanide (151-50-8); |
41. |
Potassium bifluoride (7789-29-9); |
42. |
Ammonium hydrogen fluoride or ammonium bifluoride (1341-49-7); |
43. |
Sodium fluoride (7681-49-4); |
44. |
Sodium bifluoride (1333-83-1); |
45. |
Sodium cyanide (143-33-9); |
46. |
Triethanolamine (102-71-6); |
47. |
Phosphorus pentasulphide (1314-80-3); |
48. |
Di-isopropylamine (108-18-9); |
49. |
Diethylaminoethanol (100-37-8); |
50. |
Sodium sulphide (1313-82-2); |
51. |
Sulphur monochloride (10025-67-9); |
52. |
Sulphur dichloride (10545-99-0); |
53. |
Triethanolamine hydrochloride (637-39-8); |
54. |
N,N-Diisopropyl-(Beta)-aminoethyl chloride hydrochloride (4261-68-1); |
55. |
Methylphosphonic acid (993-13-5); |
56. |
Diethyl methylphosphonate (683-08-9); |
57. |
N,N-Dimethylaminophosphoryl dichloride (677-43-0); |
58. |
Triisopropyl phosphite (116-17-6); |
59. |
Ethyldiethanolamine (139-87-7); |
60. |
O,O-Diethyl phosphorothioate (2465-65-8); |
61. |
O,O-Diethyl phosphorodithioate (298-06-6); |
62. |
Sodium hexafluorosilicate (16893-85-9); |
63. |
Methylphosphonothioic dichloride (676-98-2); |
64. |
Diethylamine (109-89-7). |
Note 1: |
For exports to "States not Party to the Chemical Weapons Convention", 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 10 % by the weight of the mixture. |
Note 2: |
For exports to "States Party to the Chemical Weapons Convention", 1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350.1, .3, .5, .11, .12, .13, .17, .18, .21, .22, .26, .27, .28, .31, .32, .33, .34, .35, .36, .54, .55, .56, .57 and .63 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture. |
Note 3: |
1C350 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C350 .2, .6, .7, .8, .9, .10, .14, .15, .16, .19, .20, .24, .25, .30, .37, .38, .39, .40, .41, .42, .43, .44, .45, .46, .47, .48, .49, .50, .51, .52, .53, .58, .59, .60, .61, .62 and .64 in which no individually specified chemical constitutes more than 30 % by the weight of the mixture. |
Note 4: |
1C350 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use. |
1C351
Human and animal pathogens and "toxins", as follows:
a. |
Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:
|
b. |
Not used; |
c. |
Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:
|
d. |
"Toxins", as follows, and "sub-unit of toxins" thereof:
|
e. |
Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:
|
Note: |
1C351 does not control "vaccines" or "immunotoxins". |
1C352
Not used
1C353
Genetic elements and genetically modified organisms, as follows:
a. |
Genetically modified organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity of organisms specified in 1C351.a., 1C351.c, 1C351.e. or 1C354; |
b. |
Genetically modified organisms or genetic elements that contain nucleic acid sequences coding for any of the "toxins" specified in 1C351.d. or "sub-units of toxins" thereof. |
Technical Notes:
1. |
Genetically-modified organisms includes organisms in which the genetic material (nucleic acid sequences) has been altered in a way that does not occur naturally by mating and/or natural recombination, and encompasses those produced artificially in whole or in part. |
2. |
Genetic elements include inter alia chromosomes, genomes, plasmids, transposons, and vectors whether genetically modified or unmodified, or chemically synthesized in whole or in part. |
3. |
Nucleic acid sequences associated with the pathogenicity of any of the micro-organisms specified in 1C351.a., 1C351.c., 1C351.e. or 1C354 means any sequence specific to the specified micro-organism that:
|
Note: |
1C353 does not control nucleic acid sequences associated with the pathogenicity of enterohaemorrhagic Escherichia coli, serotype O157 and other verotoxin producing strains, other than those coding for the verotoxin, or for its sub-units. |
1C354
Plant pathogens, as follows:
a. |
Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:
|
b. |
Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:
|
c. |
Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:
|
1C450
Toxic chemicals and toxic chemical precursors, as follows, and "chemical mixtures" containing one or more thereof:
N.B.: |
SEE ALSO ENTRY 1C350, 1C351.d. AND MILITARY GOODS CONTROLS. |
a. |
Toxic chemicals, as follows:
|
b. |
Toxic chemical precursors, as follows:
|
Note 1: |
For exports to "States not Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 10 % by the weight of the mixture. |
Note 2: |
For exports to "States Party to the Chemical Weapons Convention", 1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entries 1C450.b.1., .b.2., .b.3., .b.4., .b.5. and .b.6. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture. |
Note 3: |
1C450 does not control "chemical mixtures" containing one or more of the chemicals specified in entry 1C450.b.8. in which no individually specified chemical constitutes more than 30 % by the weight of the mixture. |
Note 4: |
1C450 does not control products identified as consumer goods packaged for retail sale for personal use or packaged for individual use. |
1D
Software
1D001
"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 1B001 to 1B003.
1D002
"Software" for the "development" of organic "matrix", metal "matrix" or carbon "matrix" laminates or "composites".
1D003
"Software" specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c. or 1A004.d.
1D101
"Software" specially designed or modified for the operation or maintenance of goods specified in 1B101, 1B102, 1B115, 1B117, 1B118 or 1B119.
1D103
"Software" specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.
1D201
"Software" specially designed for the "use" of goods specified in 1B201.
1E
Technology
1E001
"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 1A002 to 1A005, 1A006.b., 1A007, 1B or 1C.
1E002
Other "technology" as follows:
a. |
"Technology" for the "development" or "production" of polybenzothiazoles or polybenzoxazoles; |
b. |
"Technology" for the "development" or "production" of fluoroelastomer compounds containing at least one vinylether monomer; |
c. |
"Technology" for the design or "production" of the following ceramic powders or non-"composite" ceramic materials:
|
d. |
Not used. |
e. |
"Technology" for the installation, maintenance or repair of materials specified in 1C001; |
f. |
"Technology" for the repair of "composite" structures, laminates or materials specified in 1A002, 1C007.c. or 1C007.d.;
|
g. |
"Libraries" specially designed or modified to enable equipment to perform the functions of equipment specified in 1A004.c. or 1A004.d. |
1E101
"Technology" according to the General Technology Note for the "use" of goods specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1C107, 1C111 to 1C118, 1D101 or 1D103.
1E102
"Technology" according to the General Technology Note for the "development" of "software" specified in 1D001, 1D101 or 1D103.
1E103
"Technology" for the regulation of temperature, pressure or atmosphere in autoclaves or hydroclaves, when used for the "production" of "composites" or partially processed "composites".
1E104
"Technology" relating to the "production" of pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1 573 K (1 300 °C) to 3 173 K (2 900 °C) temperature range at pressures of 130 Pa to 20 kPa.
Note: |
1E104 includes "technology" for the composition of precursor gases, flow-rates and process control schedules and parameters. |
1E201
"Technology" according to the General Technology Note for the "use" of goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 to 1B234, 1C002.b.3. or .b.4., 1C010.b., 1C202, 1C210, 1C216, 1C225 to 1C241 or 1D201.
1E202
"Technology" according to the General Technology Note for the "development" or "production" of goods specified in 1A007, 1A202 or 1A225 to 1A227.
1E203
"Technology" according to the General Technology Note for the "development" of "software" specified in 1D201.
CATEGORY 2 — MATERIALS PROCESSING
2A
Systems, Equipment and Components
N.B.: |
For quiet running bearings, see the Military Goods Controls. |
2A001
Anti-friction bearings and bearing systems, as follows, and components therefor:
N.B.: |
SEE ALSO 2A101. |
Note: |
2A001 does not control balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse. |
a. |
Ball bearings and solid roller bearings, having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 4 (or national equivalents), or better, and having both rings and rolling elements (ISO 5593), made from monel or beryllium;
|
b. |
Not used; |
c. |
Active magnetic bearing systems using any of the following:
|
2A101
Radial ball bearings, other than those specified in 2A001, having all tolerances specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other national equivalents), or better and having all the following characteristics:
a. |
An inner ring bore diameter between 12 mm and 50 mm; |
b. |
An outer ring outside diameter between 25 mm and 100 mm; and |
c. |
A width between 10 mm and 20 mm. |
2A225
Crucibles made of materials resistant to liquid actinide metals, as follows:
a. |
Crucibles having both of the following characteristics:
|
b. |
Crucibles having both of the following characteristics:
|
c. |
Crucibles having all of the following characteristics:
|
2A226
Valves having all of the following characteristics:
a. |
A 'nominal size' of 5 mm or greater; |
b. |
Having a bellows seal; and |
c. |
Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight. |
Technical Note:
For valves with different inlet and outlet diameters, the 'nominal size' in 2A226 refers to the smallest diameter.
2B
Test, Inspection and Production Equipment
Technical Notes:
1. |
Secondary parallel contouring axes, (e.g., the w-axis on horizontal boring mills or a secondary rotary axis the centre line of which is parallel to the primary rotary axis) are not counted in the total number of contouring axes. Rotary axes need not rotate over 360°. A rotary axis can be driven by a linear device (e.g., a screw or a rack-and-pinion). |
2. |
For the purposes of 2B, the number of axes which can be co-ordinated simultaneously for "contouring control" is the number of axes along or around which, during processing of the workpiece, simultaneous and interrelated motions are performed between the workpiece and a tool. This does not include any additional axes along or around which other relative movement within the machine are performed such as:
|
3. |
Axis nomenclature shall be in accordance with International Standard ISO 841:2001, Industrial automation systems and integration — Numerical control of machines — Coordinate system and Motion nomenclature. |
4. |
For the purposes of 2B001 to 2B009 a "tilting spindle" is counted as a rotary axis. |
5. |
'Stated "unidirectional positioning repeatability"' may be used for each machine tool model as an alternative to individual machine tests and is determined as follows:
|
6. |
For the purposes of 2B001.a. to 2B001.c., measurement uncertainty for the "unidirectional positioning repeatability" of machine tools, as defined in the International Standard ISO 230-2:2014 or national equivalents, shall not be considered. |
7. |
For the purpose of 2B001.a. to 2B001.c., the measurement of axes shall be made according to test procedures in 5.3.2. of ISO 230-2:2014. Tests for axes longer than 2 meters shall be made over 2 m segments. Axes longer than 4 m require multiple tests (e.g., two tests for axes longer than 4 m and up to 8 m, three tests for axes longer than 8 m and up to 12 m), each over 2 m segments and distributed in equal intervals over the axis length. Test segments are equally spaced along the full axis length, with any excess length equally divided at the beginning, in between, and at the end of the test segments. The smallest "unidirectional positioning repeatability"-value of all test segments is to be reported. |
2B001
Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or "composites", which, according to the manufacturer's technical specification, can be equipped with electronic devices for "numerical control", as follows:
N.B.: |
SEE ALSO 2B201. |
Note 1: |
2B001 does not control special purpose machine tools limited to the manufacture of gears. For such machines see 2B003. |
Note 2: |
2B001 does not control special purpose machine tools limited to the manufacture of any of the following:
|
Note 3: |
A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B001.a., b. or c. |
N.B.: |
For optical finishing machines, see 2B002. |
a. |
Machine tools for turning having two or more axes which can be coordinated simultaneously for "contouring control" having any of the following:
|
b. |
Machine tools for milling having any of the following:
|
c. |
Machine tools for grinding having any of the following:
|
d. |
Electrical discharge machines (EDM) of the non-wire type which have two or more rotary axes which can be coordinated simultaneously for "contouring control"; |
e. |
Machine tools for removing metals, ceramics or "composites", having all of the following:
|
f. |
Deep-hole-drilling machines and turning machines modified for deep-hole-drilling, having a maximum depth-of-bore capability exceeding 5 m. |
2B002
Numerically controlled optical finishing machine tools equipped for selective material removal to produce non-spherical optical surfaces having all of the following characteristics:
a. |
Finishing the form to less (better) than 1,0 μm; |
b. |
Finishing to a roughness less (better) than 100 nm rms. |
c. |
Four or more axes which can be coordinated simultaneously for "contouring control"; and |
d. |
Using any of the following processes:
|
Technical Notes:
For the purposes of 2B002:
1. |
'MRF' is a material removal process using an abrasive magnetic fluid whose viscosity is controlled by a magnetic field. |
2. |
'ERF' is a removal process using an abrasive fluid whose viscosity is controlled by an electric field. |
3. |
'Energetic particle beam finishing' uses Reactive Atom Plasmas (RAP) or ion-beams to selectively remove material. |
4. |
'Inflatable membrane tool finishing' is a process that uses a pressurized membrane that deforms to contact the workpiece over a small area. |
5. |
'Fluid jet finishing' makes use of a fluid stream for material removal. |
2B003
"Numerically controlled" or manual machine tools, and specially designed components, controls and accessories therefor, specially designed for the shaving, finishing, grinding or honing of hardened (Rc = 40 or more) spur, helical and double-helical gears with a pitch diameter exceeding 1 250 mm and a face width of 15 % of pitch diameter or larger finished to a quality of AGMA 14 or better (equivalent to ISO 1328 class 3).
2B004
Hot "isostatic presses" having all of the following, and specially designed components and accessories therefor:
N.B.: |
SEE ALSO 2B104 and 2B204. |
a. |
A controlled thermal environment within the closed cavity and a chamber cavity with an inside diameter of 406 mm or more; and |
b. |
Having any of the following:
|
Technical Note:
The inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
N.B.: |
For specially designed dies, moulds and tooling see 1B003, 9B009 and the Military Goods Controls. |
2B005
Equipment specially designed for the deposition, processing and in-process control of inorganic overlays, coatings and surface modifications, as follows, for non-electronic substrates, by processes shown in the Table and associated Notes following 2E003.f., and specially designed automated handling, positioning, manipulation and control components therefor:
a. |
Chemical vapour deposition (CVD) production equipment having all of the following:
|
b. |
Ion implantation production equipment having beam currents of 5 mA or more; |
c. |
Electron beam physical vapour deposition (EB-PVD) production equipment incorporating power systems rated for over 80 kW and having any of the following:
|
d. |
Plasma spraying production equipment having any of the following:
|
e. |
Sputter deposition production equipment capable of current densities of 0,1 mA/mm2 or higher at a deposition rate of 15 μm/h or more; |
f. |
Cathodic arc deposition production equipment incorporating a grid of electromagnets for steering control of the arc spot on the cathode; |
g. |
Ion plating production equipment capable of the in situ measurement of any of the following:
|
Note: |
2B005 does not control chemical vapour deposition, cathodic arc, sputter deposition, ion plating or ion implantation equipment, specially designed for cutting or machining tools. |
2B006
Dimensional inspection or measuring systems, equipment and "electronic assemblies", as follows:
a. |
Computer controlled or "numerically controlled" Coordinate Measuring Machines (CMM), having a three dimensional (volumetric) maximum permissible error of length measurement (E0,MPE) at any point within the operating range of the machine (i.e., within the length of axes) equal to or less (better) than (1,7 + L/1 000) μm (L is the measured length in mm), according to ISO 10360-2 (2009); Technical Note: The E0,MPE of the most accurate configuration of the CMM specified by the manufacturer (e.g., best of the following: probe, stylus length, motion parameters, environment) and with "all compensations available" shall be compared to the 1,7 + L/1 000 μm threshold.
|
b. |
Linear and angular displacement measuring instruments, as follows:
|
c. |
Equipment for measuring surface roughness (including surface defects), by measuring optical scatter with a sensitivity of 0,5 nm or less (better). |
Note: |
2B006 includes machine tools, other than those specified by 2B001, that can be used as measuring machines if they meet or exceed the criteria specified for the measuring machine function. |
2B007
"Robots" having any of the following characteristics and specially designed controllers and "end-effectors" therefor:
N.B.: |
SEE ALSO 2B207. |
a. |
Capable in real time of full three-dimensional image processing or full three-dimensional 'scene analysis' to generate or modify "programmes" or to generate or modify numerical programme data; Technical Note: The 'scene analysis' limitation does not include approximation of the third dimension by viewing at a given angle, or limited grey scale interpretation for the perception of depth or texture for the approved tasks (2 1/2 D). |
b. |
Specially designed to comply with national safety standards applicable to potentially explosive munitions environments;
|
c. |
Specially designed or rated as radiation-hardened to withstand a total radiation dose greater than 5 × 103 Gy (silicon) without operational degradation; or Technical Note: The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation. |
d. |
Specially designed to operate at altitudes exceeding 30 000 m. |
2B008
Assemblies or units, specially designed for machine tools, or dimensional inspection or measuring systems and equipment, as follows:
a. |
Linear position feedback units having an overall "accuracy" less (better) than (800 + (600 × L/1 000)) nm (L equals the effective length in mm);
|
b. |
Rotary position feedback units having an "accuracy" less (better) than 0,00025°;
|
Note: |
2B008.a. and 2B008.b. control units, which are designed to determine the positioning information for feedback control, such as inductive type devices, graduated scales, infrared systems or "laser" systems. |
c. |
"Compound rotary tables" and "tilting spindles", capable of upgrading, according to the manufacturer's specifications, machine tools to or above the levels specified in 2B. |
2B009
Spin-forming machines and flow-forming machines, which, according to the manufacturer's technical specification, can be equipped with "numerical control" units or a computer control and having all of the following:
N.B.: |
SEE ALSO 2B109 AND 2B209. |
a. |
Three or more axes which can be coordinated simultaneously for "contouring control"; and |
b. |
A roller force more than 60 kN. |
Technical Note:
For the purpose of 2B009, machines combining the function of spin-forming and flow-forming are regarded as flow-forming machines.
2B104
"Isostatic presses", other than those specified in 2B004, having all of the following:
N.B.: |
SEE ALSO 2B204. |
a. |
Maximum working pressure of 69 MPa or greater; |
b. |
Designed to achieve and maintain a controlled thermal environment of 873 K (600 °C) or greater; and |
c. |
Possessing a chamber cavity with an inside diameter of 254 mm or greater. |
2B105
Chemical vapour deposition (CVD) furnaces, other than those specified in 2B005.a., designed or modified for the densification of carbon-carbon composites.
2B109
Flow-forming machines, other than those specified in 2B009, and specially designed components as follows:
N.B.: |
SEE ALSO 2B209. |
a. |
Flow-forming machines having all of the following:
|
b. |
Specially designed components for flow-forming machines specified in 2B009 or 2B109.a. |
Note: |
2B109 does not control machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for systems specified in 9A005, 9A007.a. or 9A105.a. |
Technical Note:
Machines combining the function of spin-forming and flow-forming are for the purpose of 2B109 regarded as flow-forming machines.
2B116
Vibration test systems, equipment and components therefor, as follows:
a. |
Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 10 g rms between 20 Hz and 2 kHz while imparting forces equal to or greater than 50 kN, measured 'bare table'; |
b. |
Digital controllers, combined with specially designed vibration test software, with a 'real-time control bandwidth' greater than 5 kHz designed for use with vibration test systems specified in 2B116.a.; Technical Note: In 2B116.b., 'real-time control bandwidth' means the maximum rate at which a controller can execute complete cycles of sampling, processing data and transmitting control signals. |
c. |
Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured 'bare table', and usable in vibration test systems specified in 2B116.a.; |
d. |
Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force equal to or greater than 50 kN, measured 'bare table', and usable in vibration systems specified in 2B116.a. Technical Note: In 2B116, 'bare table' means a flat table, or surface, with no fixture or fittings. |
2B117
Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B104 or 2B105, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.
2B119
Balancing machines and related equipment, as follows:
N.B.: |
SEE ALSO 2B219. |
a. |
Balancing machines having all the following characteristics:
|
b. |
Indicator heads designed or modified for use with machines specified in 2B119.a. Technical Note: Indicator heads are sometimes known as balancing instrumentation. |
2B120
Motion simulators or rate tables having all of the following characteristics:
a. |
Two axes or more; |
b. |
Designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both; and |
c. |
Having any of the following characteristics:
|
Note 1: |
2B120 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008. |
Note 2: |
Motion simulators or rate tables specified in 2B120 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export. |
2B121
Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in 2B120, having all the following characteristics:
a. |
Two axes or more; and |
b. |
A positioning "accuracy" equal to or less (better) than 5 arc second. |
Note: |
2B121 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008. |
2B122
Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both.
Note: |
Centrifuges specified in 2B122 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export. |
2B201
Machine tools and any combination thereof, other than those specified in 2B001, as follows, for removing or cutting metals, ceramics or "composites", which, according to the manufacturer's technical specification, can be equipped with electronic devices for simultaneous "contouring control" in two or more axes:
Technical Note:
Stated positioning accuracy levels derived under the following procedures from measurements made according to ISO 230-2:1988 (1) or national equivalents may be used for each machine tool model if provided to, and accepted by, national authorities instead of individual machine tests. Determination of stated positioning accuracy:
a. |
Select five machines of a model to be evaluated; |
b. |
Measure the linear axis accuracies according to ISO 230-2:1988 (1); |
c. |
Determine the accuracy values (A) for each axis of each machine. The method of calculating the accuracy value is described in the ISO 230-2:1988 (1) standard; |
d. |
Determine the average accuracy value of each axis. This average value becomes the stated positioning accuracy of each axis for the model (Âx Ây…); |
e. |
Since Item 2B201 refers to each linear axis, there will be as many stated positioning accuracy values as there are linear axes; |
f. |
If any axis of a machine tool not controlled by 2B201.a., 2B201.b. or 2B201.c. has a stated positioning accuracy of 6 μm or better (less) for grinding machines, and 8 μm or better (less) for milling and turning machines, both according to ISO 230-2:1988 (1), then the builder should be required to reaffirm the accuracy level once every eighteen months. |
a. |
Machine tools for milling, having any of the following characteristics:
|
b. |
Machine tools for grinding, having any of the following characteristics:
|
c. |
Machine tools for turning, that have positioning accuracies with "all compensations available" better (less) than 6 μm according to ISO 230-2:1988 (2) along any linear axis (overall positioning) for machines capable of machining diameters greater than 35 mm;
|
Note 1: |
2B201 does not control special purpose machine tools limited to the manufacture of any of the following parts:
|
Note 2: |
A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry 2B201.a., b. or c. |
Note 3: |
Items 2B201a.3. and 2B201b.3. include machines based on a parallel linear kinematic design (e.g., hexapods) that have 5 or more axes none of which are rotary axes. |
2B204
"Isostatic presses", other than those specified in 2B004 or 2B104, and related equipment, as follows:
a. |
"Isostatic presses" having both of the following characteristics:
|
b. |
Dies, moulds and controls, specially designed for "isostatic presses" specified in 2B204.a. |
Technical Note:
In 2B204 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not include fixtures. That dimension will be the smaller of either the inside diameter of the pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other.
2B206
Dimensional inspection machines, instruments or systems, other than those specified in 2B006, as follows:
a. |
Computer controlled or numerically controlled coordinate measuring machines (CMM) having either of the following characteristics:
Technical Note: The E0,MPE of the most accurate configuration of the CMM specified according to ISO 10360-2(2009) by the manufacturer (e.g., best of the following: probe, stylus, length, motion parameters, environments) and with all compensations available shall be compared to the 1,7 + L/800 μm threshold. |
b. |
Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:
|
c. |
'Linear displacement' measuring systems having all of the following characteristics: Technical Note: For the purpose of 2B206.c. 'linear displacement' means the change of distance between the measuring probe and the measured object.
|
Note 1: |
Machine tools that can be used as measuring machines are controlled if they meet or exceed the criteria specified for the machine tool function or the measuring machine function. |
Note 2: |
A machine specified in 2B206 is controlled if it exceeds the control threshold anywhere within its operating range. |
Technical Notes:
All parameters of measurement values in 2B206 represent plus/minus i.e., not total band.
2B207
"Robots", "end-effectors" and control units, other than those specified in 2B007, as follows:
a. |
"Robots" or "end-effectors" specially designed to comply with national safety standards applicable to handling high explosives (for example, meeting electrical code ratings for high explosives); |
b. |
Control units specially designed for any of the "robots" or "end-effectors" specified in 2B207.a. |
2B209
Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in 2B009 or 2B109, and mandrels, as follows:
a. |
Machines having both of the following characteristics:
|
b. |
Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm. |
Note: |
2B209.a. includes machines which have only a single roller designed to deform metal plus two auxiliary rollers which support the mandrel, but do not participate directly in the deformation process. |
2B219
Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:
a. |
Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:
|
b. |
Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:
|
2B225
Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, having either of the following characteristics:
a. |
A capability of penetrating 0,6 m or more of hot cell wall (through-the-wall operation); or |
b. |
A capability of bridging over the top of a hot cell wall with a thickness of 0,6 m or more (over-the-wall operation). |
Technical Note:
Remote manipulators provide translation of human operator actions to a remote operating arm and terminal fixture. They may be of 'master/slave' type or operated by joystick or keypad.
2B226
Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:
N.B: |
SEE ALSO 3B. |
a. |
Furnaces having all of the following characteristics:
|
b. |
Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in 2B226.a. |
Note: |
2B226.a. does not control furnaces designed for the processing of semiconductor wafers. |
2B227
Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:
a. |
Arc remelt and casting furnaces having both of the following characteristics:
|
b. |
Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:
|
c. |
Computer control and monitoring systems specially configured for any of the furnaces specified in 2B227.a. or b. |
2B228
Rotor fabrication or assembly equipment, rotor straightening equipment, bellows-forming mandrels and dies, as follows:
a. |
Rotor assembly equipment for assembly of gas centrifuge rotor tube sections, baffles, and end caps;
|
b. |
Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis; Technical Note: In 2B228.b. such equipment normally consists of precision measuring probes linked to a computer that subsequently controls the action of, for example, pneumatic rams used for aligning the rotor tube sections. |
c. |
Bellows-forming mandrels and dies for producing single-convolution bellows. Technical Note: In 2B228.c. the bellows have all of the following characteristics:
|
2B230
All types of 'pressure transducers' capable of measuring absolute pressures and having all of the following:
a. |
Pressure sensing elements made of or protected by aluminium, aluminium alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers; |
b. |
Seals, if any, essential for sealing the pressure sensing element, and in direct contact with the process medium, made of or protected by aluminium, aluminium alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with more than 60 % nickel by weight, or fully fluorinated hydrocarbon polymers; and |
c. |
Having either of the following characteristics:
|
Technical Notes:
1. |
In 2B230 'pressure transducer' means a device that converts a pressure measurement into a signal. |
2. |
For the purposes of 2B230, 'accuracy' includes non-linearity, hysteresis and repeatability at ambient temperature. |
2B231
Vacuum pumps having all of the following characteristics:
a. |
Input throat size equal to or greater than 380 mm; |
b. |
Pumping speed equal to or greater than 15 m3/s; and |
c. |
Capable of producing an ultimate vacuum better than 13 mPa. |
Technical Notes:
1. |
The pumping speed is determined at the measurement point with nitrogen gas or air. |
2. |
The ultimate vacuum is determined at the input of the pump with the input of the pump blocked off. |
2B232
High-velocity gun systems (propellant, gas, coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 1,5 km/s or greater.
N.B.: |
SEE ALSO MILTARY GOODS CONTROLS. |
2B233
Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following:
N.B.: |
SEE ALSO 2B350.i. |
a. |
Capable of an inlet volume flow rate of 50 m3/h or greater; |
b. |
Capable of a pressure ratio of 2:1 or greater; and |
c. |
Having all surfaces that come in contact with the process gas made from any of the following materials:
|
2B350
Chemical manufacturing facilities, equipment and components, as follows:
a. |
Reaction vessels or reactors, with or without agitators, with total internal (geometric) volume greater than 0,1 m3 (100 litres) and less than 20 m3 (20 000 litres), where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:
|
b. |
Agitators designed for use in reaction vessels or reactors specified in 2B350.a.; and impellers, blades or shafts designed for such agitators, where all surfaces of the agitator that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:
|
c. |
Storage tanks, containers or receivers with a total internal (geometric) volume greater than 0,1 m3 (100 litres) where all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:
|
d. |
Heat exchangers or condensers with a heat transfer surface area greater than 0,15 m2, and less than 20 m2; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:
|
e. |
Distillation or absorption columns of internal diameter greater than 0,1 m; and liquid distributors, vapour distributors or liquid collectors designed for such distillation or absorption columns, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:
|
f. |
Remotely operated filling equipment in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:
|
g. |
Valves and components, as follows:
Technical Notes:
|
h. |
Multi-walled piping incorporating a leak detection port, in which all surfaces that come in direct contact with the chemical(s) being processed or contained are made from any of the following materials:
|
i. |
Multiple-seal and seal-less pumps, with manufacturer's specified maximum flow-rate greater than 0,6 m3/hour, or vacuum pumps with manufacturer's specified maximum flow-rate greater than 5 m3/hour (under standard temperature (273 K (0 °C)) and pressure (101,3 kPa) conditions), other than those specified in 2B233; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:
Technical Note: In 2B350.i., the term seal refers to only those seals that come into direct contact with the chemical(s) being processed (or are designed to), and provide a sealing function where a rotary or reciprocating drive shaft passes through a pump body. |
j. |
Incinerators designed to destroy chemicals specified in entry 1C350, having specially designed waste supply systems, special handling facilities and an average combustion chamber temperature greater than 1 273 K (1 000 °C), in which all surfaces in the waste supply system that come into direct contact with the waste products are made from or lined with any of the following materials:
|
Note: |
For the purposes of 2B350, the materials used for gaskets, packing, seals, screws, washers or other materials performing a sealing function do not determine the status of control, provided that such components are designed to be interchangeable. |
Technical Notes:
1. |
'Carbon graphite' is a composition consisting of amorphous carbon and graphite, in which the graphite content is eight percent or more by weight. |
2. |
For the listed materials in the above entries, the term 'alloy' when not accompanied by a specific elemental concentration is understood as identifying those alloys where the identified metal is present in a higher percentage by weight than any other element. |
2B351
Toxic gas monitoring systems and their dedicated detecting components, other than those specified in 1A004, as follows; and detectors; sensor devices; and replaceable sensor cartridges therefor:
a. |
Designed for continuous operation and usable for the detection of chemical warfare agents or chemicals specified in 1C350, at concentrations of less than 0,3 mg/m3; or |
b. |
Designed for the detection of cholinesterase-inhibiting activity. |
2B352
Equipment capable of use in handling biological materials, as follows:
a. |
Complete biological containment facilities at P3, P4 containment level; Technical Note: P3 or P4 (BL3, BL4, L3, L4) containment levels are as specified in the WHO Laboratory Biosafety manual (3rd edition Geneva 2004). |
b. |
Fermenters and components as follows:
Technical Note: For the purposes of 2B352.b. fermenters include bioreactors, single-use (disposable) bioreactors, chemostats and continuous-flow systems. |
c. |
Centrifugal separators, capable of continuous separation without the propagation of aerosols, having all the following characteristics:
Technical Note: Centrifugal separators include decanters. |
d. |
Cross (tangential) flow filtration equipment capable of separation of pathogenic micro-organisms, viruses, toxins or cell cultures having all the following characteristics:
|
e. |
Steam, gas or vapour sterilisable freeze-drying equipment with a condenser capacity of 10 kg of ice or more in 24 hours and less than 1 000 kg of ice in 24 hours; |
f. |
Protective and containment equipment, as follows:
|
g. |
Aerosol inhalation equipment designed for aerosol challenge testing with "microorganisms", "viruses" or "toxins" as follows:
|
h. |
Spray drying equipment capable of drying toxins or pathogenic microorganisms having all of the following:
|
2C
Materials
None.
2D
Software
2D001
"Software", other than that specified in 2D002, as follows:
a. |
"Software" specially designed or modified for the "development" or "production" of equipment specified in 2A001 or 2B001 |
b. |
"Software" specially designed or modified for the "use" of equipment specified in 2A001.c, 2B001 or 2B003 to 2B009. |
Note: |
2D001 does not control part programming "software" that generates "numerical control" codes for machining various parts. |
2D002
"Software" for electronic devices, even when residing in an electronic device or system, enabling such devices or systems to function as a "numerical control" unit, capable of co-ordinating simultaneously more than four axes for "contouring control".
Note 1: |
2D002 does not control "software" specially designed or modified for the operation of items not specified in Category 2. |
Note 2: |
2D002 does not control "software" for items specified in 2B002. See 2D001 and 2D003 for "software" for items specified in 2B002. |
Note 3: |
2D002 does not control "software" that is exported with, and the minimum necessary for the operation of, items not specified by Category 2. |
2D003
"Software", designed or modified for the operation of equipment specified in 2B002, that converts optical design, workpiece measurements and material removal functions into "numerical control" commands to achieve the desired workpiece form.
2D101
"Software" specially designed or modified for the "use" of equipment specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122.
N.B.: |
SEE ALSO 9D004. |
2D201
"Software" specially designed for the "use" of equipment specified in 2B204, 2B206, 2B207, 2B209, 2B219 or 2B227.
2D202
"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 2B201.
Note: |
2D202 does not control part programming "software" that generates "numerical control" command codes but does not allow direct use of equipment for machining various parts. |
2D351
"Software", other than that specified in 1D003, specially designed for "use" of equipment specified in 2B351.
2E
Technology
2E001
"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 2A, 2B or 2D.
Note: |
2E001 includes "technology" for the integration of probe systems into coordinate measurement machines specified in 2B006.a. |
2E002
"Technology" according to the General Technology Note for the "production" of equipment specified in 2A or 2B.
2E003
Other "technology", as follows:
a. |
"Technology" for the "development" of interactive graphics as an integrated part in "numerical control" units for preparation or modification of part programmes; |
b. |
"Technology" for metal-working manufacturing processes, as follows:
|
c. |
"Technology" for the "development" or "production" of hydraulic stretch-forming machines and dies therefor, for the manufacture of airframe structures; |
d. |
"Technology" for the "development" of generators of machine tool instructions (e.g., part programmes) from design data residing inside "numerical control" units; |
e. |
"Technology" for the "development" of integration "software" for incorporation of expert systems for advanced decision support of shop floor operations into "numerical control" units; |
f. |
"Technology" for the application of inorganic overlay coatings or inorganic surface modification coatings (specified in column 3 of the following table) to non-electronic substrates (specified in column 2 of the following table), by processes specified in column 1 of the following table and defined in the Technical Note.
|
2E101
"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B119 to 2B122 or 2D101.
2E201
"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 2A225, 2A226, 2B001, 2B006, 2B007.b., 2B007.c., 2B008, 2B009, 2B201, 2B204, 2B206, 2B207, 2B209, 2B225 to 2B233, 2D201 or 2D202.
2E301
"Technology" according to the General Technology Note for the "use" of goods specified in 2B350 to 2B352.
Table
Deposition techniques
|
|
|
||||||
|
"Superalloys" |
Aluminides for internal passages |
||||||
|
Ceramics (19) and Low expansion glasses (14) |
Silicides Carbides Dielectric layers (15) Diamond Diamond-like carbon (17) |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Silicides Carbides Refractory metals Mixtures thereof (4) Dielectric layers (15) Aluminides Alloyed aluminides (2) Boron nitride |
||||||
|
Cemented tungsten carbide (16), Silicon carbide (18) |
Carbides Tungsten Mixtures thereof (4) Dielectric layers (15) |
||||||
|
Molybdenum and Molybdenum alloys |
Dielectric layers (15) |
||||||
|
Beryllium and Beryllium alloys |
Dielectric layers (15) Diamond Diamond-like carbon (17) |
||||||
|
Sensor window materials (9) |
Dielectric layers (15) Diamond Diamond-like carbon (17) |
||||||
Thermal-Evaporation Physical Vapour Deposition (TE-PVD) |
|
|
||||||
|
"Superalloys" |
Alloyed silicides Alloyed aluminides (2) MCrAlX (5) Modified zirconia (12) Silicides Aluminides Mixtures thereof (4) |
||||||
|
Ceramics (19) and Low expansion glasses (14) |
Dielectric layers (15) |
||||||
|
Corrosion resistant steel (7) |
MCrAlX (5) Modified zirconia (12) Mixtures thereof (4) |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Silicides Carbides Refractory metals Mixtures thereof (4) Dielectric layers (15) Boron nitride |
||||||
|
Cemented tungsten carbide (16), Silicon carbide (18) |
Carbides Tungsten Mixtures thereof (4) Dielectric layers (15) |
||||||
|
Molybdenum and Molybdenum alloys |
Dielectric layers (15) |
||||||
|
Beryllium and Beryllium alloys |
Dielectric layers (15) Borides Beryllium |
||||||
|
Sensor window materials (9) |
Dielectric layers (15) |
||||||
|
Titanium alloys (13) |
Borides Nitrides |
||||||
|
Ceramics (19) and Low-expansion glasses |
Dielectric layers (15) Diamond-like carbon (17) |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Dielectric layers (15) |
||||||
|
Cemented tungsten carbide (16), Silicon carbide |
Dielectric layers (15) |
||||||
|
Molybdenum and Molybdenum alloys |
Dielectric layers (15) |
||||||
|
Beryllium and Beryllium alloys |
Dielectric layers (15) |
||||||
|
Sensor window materials (9) |
Dielectric layers (15) Diamond-like carbon (17) |
||||||
|
Ceramics (19) and Low expansion glasses (14) |
Silicides Dielectric layers (15) Diamond-like carbon (17) |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Dielectric layers (15) |
||||||
|
Cemented tungsten carbide (16), Silicon carbide |
Dielectric layers (15) |
||||||
|
Molybdenum and Molybdenum alloys |
Dielectric layers (15) |
||||||
|
Beryllium and Beryllium alloys |
Dielectric layers (15) |
||||||
|
Sensor window materials (9) |
Dielectric layers (15) Diamond-like carbon |
||||||
|
"Superalloys" |
Alloyed silicides Alloyed aluminides (2) MCrAlX (5) |
||||||
|
Polymers (11) and Organic "matrix""composites" |
Borides Carbides Nitrides Diamond-like carbon (17) |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Silicides Carbides Mixtures thereof (4) |
||||||
|
Titanium alloys (13) |
Silicides Aluminides Alloyed aluminides (2) |
||||||
|
Refractory metals and alloys (8) |
Silicides Oxides |
||||||
|
"Superalloys" |
MCrAlX (5) Modified zirconia (12) Mixtures thereof (4) Abradable Nickel-Graphite Abradable materials containing Ni-Cr-Al Abradable Al-Si-Polyester Alloyed aluminides (2) |
||||||
|
Aluminium alloys (6) |
MCrAlX (5) Modified zirconia (12) Silicides Mixtures thereof (4) |
||||||
|
Refractory metals and alloys (8) |
Aluminides Silicides Carbides |
||||||
|
Corrosion resistant steel (7) |
MCrAlX (5) Modified zirconia (12) Mixtures thereof (4) |
||||||
|
Titanium alloys (13) |
Carbides Aluminides Silicides Alloyed aluminides (2) Abradable Nickel-Graphite Abradable materials containing Ni-Cr-Al Abradable Al-Si-Polyester |
||||||
|
Refractory metals and alloys (8) |
Fused silicides Fused aluminides except for resistance heating elements |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Silicides Carbides Mixtures thereof (4) |
||||||
|
"Superalloys" |
Alloyed silicides Alloyed aluminides (2) Noble metal modified aluminides (3) MCrAlX (5) Modified zirconia (12) Platinum Mixtures thereof (4) |
||||||
|
Ceramics and Low- expansion glasses (14) |
Silicides Platinum Mixtures thereof (4) Dielectic layers (15) Diamond-like carbon (17) |
||||||
|
Titanium alloys (13) |
Borides Nitrides Oxides Silicides Aluminides Alloyed aluminides (2) Carbides |
||||||
|
Carbon-carbon, Ceramic and Metal "matrix""composites" |
Silicides Carbides Refractory metals Mixtures thereof (4) Dielectric layers (15) Boron nitride |
||||||
|
Cemented tungsten carbide (16), Silicon carbide (18) |
Carbides Tungsten Mixtures thereof (4) Dielectric layers (15) Boron nitride |
||||||
|
Molybdenum and Molybdenum alloys |
Dielectric layers (15) |
||||||
|
Beryllium and Beryllium alloys |
Borides Dielectric layers (15) Beryllium |
||||||
|
Sensor window materials (9) |
Dielectric layers (15) Diamond-like carbon (17) |
||||||
|
Refractory metals and alloys (8) |
Aluminides Silicides Oxides Carbides |
||||||
|
High temperature bearing steels |
Additions of Chromium Tantalum or Niobium (Columbium) |
||||||
|
Titanium alloys (13) |
Borides Nitrides |
||||||
|
Beryllium and Beryllium alloys |
Borides |
||||||
|
Cemented tungsten carbide (16) |
Carbides Nitrides |
TABLE — DEPOSITION TECHNIQUES — NOTES
1. |
The term 'coating process' includes coating repair and refurbishing as well as original coating. |
2. |
The term 'alloyed aluminide coating' includes single or multiple-step coatings in which an element or elements are deposited prior to or during application of the aluminide coating, even if these elements are deposited by another coating process. It does not, however, include the multiple use of single-step pack cementation processes to achieve alloyed aluminides. |
3. |
The term 'noble metal modified aluminide' coating includes multiple-step coatings in which the noble metal or noble metals are laid down by some other coating process prior to application of the aluminide coating. |
4. |
The term 'mixtures thereof' includes infiltrated material, graded compositions, co-deposits and multilayer deposits and are obtained by one or more of the coating processes specified in the Table. |
5. |
'MCrAlX' refers to a coating alloy where M equals cobalt, iron, nickel or combinations thereof and X equals hafnium, yttrium, silicon, tantalum in any amount or other intentional additions over 0,01 % by weight in various proportions and combinations, except:
|
6. |
The term 'aluminium alloys' refers to alloys having an ultimate tensile strength of 190 MPa or more measured at 293 K (20 °C). |
7. |
The term 'corrosion resistant steel' refers to AISI (American Iron and Steel Institute) 300 series or equivalent national standard steels. |
8. |
'Refractory metals and alloys' include the following metals and their alloys: niobium (columbium), molybdenum, tungsten and tantalum. |
9. |
'Sensor window materials', as follows: alumina, silicon, germanium, zinc sulphide, zinc selenide, gallium arsenide, diamond, gallium phosphide, sapphire and the following metal halides: sensor window materials of more than 40 mm diameter for zirconium fluoride and hafnium fluoride. |
10. |
"Technology" for single-step pack cementation of solid airfoils is not controlled by Category 2. |
11. |
'Polymers', as follows: polyimide, polyester, polysulphide, polycarbonates and polyurethanes. |
12. |
'Modified zirconia' refers to additions of other metal oxides (e.g., calcia, magnesia, yttria, hafnia, rare earth oxides) to zirconia in order to stabilise certain crystallographic phases and phase compositions. Thermal barrier coatings made of zirconia, modified with calcia or magnesia by mixing or fusion, are not controlled. |
13. |
'Titanium alloys' refers only to aerospace alloys having an ultimate tensile strength of 900 MPa or more measured at 293 K (20 °C). |
14. |
'Low-expansion glasses' refers to glasses which have a coefficient of thermal expansion of 1 × 10– 7 K– 1 or less measured at 293 K (20 °C). |
15. |
'Dielectric layers' are coatings constructed of multi-layers of insulator materials in which the interference properties of a design composed of materials of various refractive indices are used to reflect, transmit or absorb various wavelength bands. Dielectric layers refers to more than four dielectric layers or dielectric/metal "composite" layers. |
16. |
'Cemented tungsten carbide' does not include cutting and forming tool materials consisting of tungsten carbide/(cobalt, nickel), titanium carbide/(cobalt, nickel), chromium carbide/nickel-chromium and chromium carbide/nickel. |
17. |
"Technology" specially designed to deposit diamond-like carbon on any of the following is not controlled: magnetic disk drives and heads, equipment for the manufacture of disposables, valves for faucets, acoustic diaphragms for speakers, engine parts for automobiles, cutting tools, punching-pressing dies, office automation equipment, microphones or medical devices or moulds, for casting or moulding of plastics, manufactured from alloys containing less than 5 % beryllium. |
18. |
'Silicon carbide' does not include cutting and forming tool materials. |
19. |
Ceramic substrates, as used in this entry, does not include ceramic materials containing 5 % by weight, or greater, clay or cement content, either as separate constituents or in combination. |
TABLE — DEPOSITION TECHNIQUES — TECHNICAL NOTE
Processes specified in Column 1 of the Table are defined as follows:
a. |
Chemical Vapour Deposition (CVD) is an overlay coating or surface modification coating process wherein a metal, alloy, "composite", dielectric or ceramic is deposited upon a heated substrate. Gaseous reactants are decomposed or combined in the vicinity of a substrate resulting in the deposition of the desired elemental, alloy or compound material on the substrate. Energy for this decomposition or chemical reaction process may be provided by the heat of the substrate, a glow discharge plasma, or "laser" irradiation.
|
b. |
Thermal Evaporation-Physical Vapour Deposition (TE-PVD) is an overlay coating process conducted in a vacuum with a pressure less than 0,1 Pa wherein a source of thermal energy is used to vaporize the coating material. This process results in the condensation, or deposition, of the evaporated species onto appropriately positioned substrates. The addition of gases to the vacuum chamber during the coating process to synthesize compound coatings is an ordinary modification of the process. The use of ion or electron beams, or plasma, to activate or assist the coating's deposition is also a common modification in this technique. The use of monitors to provide in-process measurement of optical characteristics and thickness of coatings can be a feature of these processes. Specific TE-PVD processes are as follows:
|
c. |
Pack Cementation is a surface modification coating or overlay coating process wherein a substrate is immersed in a powder mixture (a pack), that consists of:
The substrate and powder mixture is contained within a retort which is heated to between 1 030 K (757 °C) and 1 375 K (1 102 °C) for sufficient time to deposit the coating. |
d. |
Plasma Spraying is an overlay coating process wherein a gun (spray torch) which produces and controls a plasma accepts powder or wire coating materials, melts them and propels them towards a substrate, whereon an integrally bonded coating is formed. Plasma spraying constitutes either low pressure plasma spraying or high velocity plasma spraying.
|
e. |
Slurry Deposition is a surface modification coating or overlay coating process wherein a metallic or ceramic powder with an organic binder is suspended in a liquid and is applied to a substrate by either spraying, dipping or painting, subsequent air or oven drying, and heat treatment to obtain the desired coating. |
f. |
Sputter Deposition is an overlay coating process based on a momentum transfer phenomenon, wherein positive ions are accelerated by an electric field towards the surface of a target (coating material). The kinetic energy of the impacting ions is sufficient to cause target surface atoms to be released and deposited on an appropriately positioned substrate.
|
g. |
Ion Implantation is a surface modification coating process in which the element to be alloyed is ionized, accelerated through a potential gradient and implanted into the surface region of the substrate. This includes processes in which ion implantation is performed simultaneously with electron beam physical vapour deposition or sputter deposition. |
CATEGORY 3 — ELECTRONICS
3A
Systems, Equipment and Components
Note 1: |
The control status of equipment and components described in 3A001 or 3A002, other than those described in 3A001.a.3. to 3A001.a.10., 3A001.a.12. or 3A001.a.13, which are specially designed for or which have the same functional characteristics as other equipment is determined by the control status of the other equipment. |
Note 2: |
The control status of integrated circuits described in 3A001.a.3. to 3A001.a.9., 3A001.a.12. or 3A001.a.13 which are unalterably programmed or designed for a specific function for another equipment is determined by the control status of the other equipment.
|
3A001
Electronic items as follows:
a. |
General purpose integrated circuits, as follows:
|
b. |
Microwave or millimetre wave items as follows: Technical Note: For purposes of 3A001.b., the parameter peak saturated power output may also be referred to on product data sheets as output power, saturated power output, maximum power output, peak power output, or peak envelope power output.
|
c. |
Acoustic wave devices as follows and specially designed components therefor:
|
d. |
Electronic devices and circuits containing components, manufactured from "superconductive" materials, specially designed for operation at temperatures below the "critical temperature" of at least one of the "superconductive" constituents and having any of the following:
|
e. |
High energy devices as follows:
|
f. |
Rotary input type absolute position encoders having an "accuracy" equal to or less (better) than 1,0 second of arc; |
g. |
Solid-state pulsed power switching thyristor devices and 'thyristor modules', using either electrically, optically, or electron radiation controlled switch methods and having any of the following:
Technical Note: For the purposes of 3A001.g., a 'thyristor module' contains one or more thyristor devices. |
h. |
Solid-state power semiconductor switches, diodes, or 'modules', having all of the following:
Technical Note: For the purposes of 3A001.h., 'modules' contain one or more solid-state power semiconductor switches or diodes. |
3A002
General purpose "electronic assemblies", modules and equipment, as follows:
a. |
Recording equipment and oscilloscopes as follows:
|
b. |
Not used; |
c. |
"Signal analysers" as follows:
|
d. |
Signal generators having any of the following:
Technical Notes:
|
e. |
Network analysers having any of the following:
|
f. |
Microwave test receivers having all of the following:
|
g. |
Atomic frequency standards being any of the following:
|
h. |
"Electronic assemblies", modules, or equipment, specified to perform all of the following:
Technical Note: For multiple-channel "electronic assemblies" or modules, control status is determined by the highest single-channel specified performance.
|
3A003
Spray cooling thermal management systems employing closed loop fluid handling and reconditioning equipment in a sealed enclosure where a dielectric fluid is sprayed onto electronic components using specially designed spray nozzles that are designed to maintain electronic components within their operating temperature range, and specially designed components therefor.
3A101
Electronic equipment, devices and components, other than those specified in 3A001, as follows:
a. |
Analogue-to-digital converters, usable in "missiles", designed to meet military specifications for ruggedized equipment; |
b. |
Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and systems containing those accelerators.
|
3A102
'Thermal batteries' designed or modified for 'missiles'.
Technical Notes:
1. |
In 3A102 'thermal batteries' are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery. |
2. |
In 3A102 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
3A201
Electronic components, other than those specified in 3A001, as follows;
a. |
Capacitors having either of the following sets of characteristics:
|
b. |
Superconducting solenoidal electromagnets having all of the following characteristics:
|
c. |
Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:
Technical Notes:
|
3A225
Frequency changers or generators, other than those specified in 0B001.b.13., usable as a variable or fixed frequency motor drive, having all of the following characteristics:
N.B. 1: |
"Software" specially designed to enhance or release the performance of a frequency changer or generator to meet the characteristics of 3A225 is specified in 3D225. |
N.B. 2: |
"Technology" in the form of codes or keys to enhance or release the performance of a frequency changer or generator to meet the characteristics of 3A225 is specified in 3E225. |
a. |
Multiphase output providing a power of 40 VA or greater; |
b. |
Operating at a frequency of 600 Hz or more; and |
c. |
Frequency control better (less) than 0,2 %. |
Note: |
3A225 does not control frequency changers or generators if they have hardware, "software" or "technology" constraints that limit the performance to less than that specified above, provided they meet any of the following:
|
Technical Notes:
1. |
Frequency changers in 3A225 are also known as converters or inverters. |
2. |
Frequency changers in 3A225 may be marketed as Generators, Electronic Test Equipment, AC Power Supplies, Variable Speed Motors Drives, Variable Speed Drives (VSDs), Variable Frequency Drives (VFDs), Adjustable Frequency Drives (AFDs), or Adjustable Speed Drives (ASDs). |
3A226
High-power direct current power supplies, other than those specified in 0B001.j.6., having both of the following characteristics:
a. |
Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; and |
b. |
Current or voltage stability better than 0,1 % over a time period of 8 hours. |
3A227
High-voltage direct current power supplies, other than those specified in 0B001.j.5., having both of the following characteristics:
a. |
Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; and |
b. |
Current or voltage stability better than 0,1 % over a time period of 8 hours. |
3A228
Switching devices, as follows:
a. |
Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:
|
b. |
Triggered spark-gaps having both of the following characteristics:
|
c. |
Modules or assemblies with a fast switching function, other than those specified in 3A001.g. or 3A001.h., having all of the following characteristics:
|
3A229
High-current pulse generators as follows:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS. |
a. |
Detonator firing sets (initiator systems, firesets), including electronically-charged, explosively-driven and optically-driven firing sets, other than those specified in 1A007.a., designed to drive multiple controlled detonators specified in 1A007.b.; |
b. |
Modular electrical pulse generators (pulsers) having all of the following characteristics:
|
c. |
Micro-firing units having all of the following characteristics:
|
3A230
High-speed pulse generators, and 'pulse heads' therefor, having both of the following characteristics:
a. |
Output voltage greater than 6 V into a resistive load of less than 55 ohms, and |
b. |
'Pulse transition time' less than 500 ps. |
Technical Notes:
1. |
In 3A230, 'pulse transition time' is defined as the time interval between 10 % and 90 % voltage amplitude. |
2. |
'Pulse heads' are impulse forming networks designed to accept a voltage step function and shape it into a variety of pulse forms that can include rectangular, triangular, step, impulse, exponential, or monocycle types. 'Pulse heads' can be an integral part of the pulse generator, they can be a plug-in module to the device or they can be an externally connected device. |
3A231
Neutron generator systems, including tubes, having both of the following characteristics:
a. |
Designed for operation without an external vacuum system; and |
b. |
Utilizing any of the following:
|
3A232
Multipoint initiation systems, other than those specified in 1A007, as follows:
N.B.: |
SEE ALSO MILITARY GOODS CONTROLS. |
N.B.: |
See 1A007.b. for detonators. |
a. |
Not used; |
b. |
Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over an area greater than 5 000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2,5 μs. |
Note: |
3A232 does not control detonators using only primary explosives, such as lead azide. |
3A233
Mass spectrometers, other than those specified in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:
a. |
Inductively coupled plasma mass spectrometers (ICP/MS); |
b. |
Glow discharge mass spectrometers (GDMS); |
c. |
Thermal ionization mass spectrometers (TIMS); |
d. |
Electron bombardment mass spectrometers having both of the following features:
|
e. |
Not used; |
f. |
Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides. |
Technical Notes:
1. |
Electron bombardment mass spectrometers in 3A233.d. are also known as electron impact mass spectrometers or electron ionization mass spectrometers. |
2. |
In 3A233.d.2., a 'cold trap' is a device that traps gas molecules by condensing or freezing them on cold surfaces. For the purposes of 3A233.d.2., a closed-loop gaseous helium cryogenic vacuum pump is not a 'cold trap'. |
3A234
Striplines to provide low inductance path to detonators with the following characteristics:
a. |
Voltage rating greater than 2 kV; and |
b |
Inductance of less than 20 nH. |
3B
Test, Inspection and Production Equipment
3B001
Equipment for the manufacturing of semiconductor devices or materials, as follows and specially designed components and accessories therefor:
a. |
Equipment designed for epitaxial growth as follows:
|
b. |
Equipment designed for ion implantation and having any of the following:
|
c. |
Not used; |
d. |
Not used; |
e. |
Automatic loading multi-chamber central wafer handling systems having all of the following:
Technical Notes:
|
f. |
Lithography equipment as follows:
|
g. |
Masks and reticles, designed for integrated circuits specified in 3A001; |
h. |
Multi-layer masks with a phase shift layer not specified by 3B001.g. and having any of the following:
|
i. |
Imprint lithography templates designed for integrated circuits specified in 3A001. |
3B002
Test equipment specially designed for testing finished or unfinished semiconductor devices as follows and specially designed components and accessories therefor:
a. |
For testing S-parameters of transistor devices at frequencies exceeding 31,8 GHz; |
b. |
Not used; |
c. |
For testing microwave integrated circuits specified in 3A001.b.2. |
3C
Materials
3C001
Hetero-epitaxial materials consisting of a "substrate" having stacked epitaxially grown multiple layers of any of the following:
a. |
Silicon (Si); |
b. |
Germanium (Ge); |
c. |
Silicon carbide (SiC); or |
d. |
"III/V compounds" of gallium or indium. |
Note: |
3C001.d. does not control a "substrate" having one or more P-type epitaxial layers of GaN, InGaN, AlGaN, InAlN, InAlGaN, GaP, InGaP, AlInP or InGaAlP, independent of the sequence of the elements, except if the P-type epitaxial layer is between N-type layers. |
3C002
Resist materials as follows and "substrates" coated with the following resists:
a. |
Resists designed for semiconductor lithography as follows:
|
b. |
All resists designed for use with electron beams or ion beams, with a sensitivity of 0,01 μcoulomb/mm2 or better; |
c. |
Not used; |
d. |
All resists optimised for surface imaging technologies; |
e. |
All resists designed or optimised for use with imprint lithography equipment specified in 3B001.f.2. that use either a thermal or photo-curable process. |
3C003
Organo-inorganic compounds as follows:
a. |
Organo-metallic compounds of aluminium, gallium or indium, having a purity (metal basis) better than 99,999 %; |
b. |
Organo-arsenic, organo-antimony and organo-phosphorus compounds, having a purity (inorganic element basis) better than 99,999 %. |
Note: |
3C003 only controls compounds whose metallic, partly metallic or non-metallic element is directly linked to carbon in the organic part of the molecule. |
3C004
Hydrides of phosphorus, arsenic or antimony, having a purity better than 99,999 %, even diluted in inert gases or hydrogen.
Note: |
3C004 does not control hydrides containing 20 % molar or more of inert gases or hydrogen. |
3C005
Silicon carbide (SiC), gallium nitride (GaN), aluminium nitride (AlN) or aluminium gallium nitride (AlGaN) semiconductor "substrates", or ingots, boules, or other preforms of those materials, having resistivities greater than 10 000 ohm-cm at 20 °C.
3C006
"Substrates" specified in 3C005 with at least one epitaxial layer of silicon carbide, gallium nitride, aluminium nitride or aluminium gallium nitride.
3D
Software
3D001
"Software" specially designed for the "development" or "production" of equipment specified in 3A001.b. to 3A002.h. or 3B.
3D002
"Software" specially designed for the "use" of equipment specified in 3B001.a. to f., 3B002 or 3A225
3D003
'Physics-based' simulation "software" specially designed for the "development" of lithographic, etching or deposition processes for translating masking patterns into specific topographical patterns in conductors, dielectrics or semiconductor materials.
Technical Note:
'Physics-based' in 3D003 means using computations to determine a sequence of physical cause and effect events based on physical properties (e.g., temperature, pressure, diffusion constants and semiconductor materials properties).
Note: |
Libraries, design attributes or associated data for the design of semiconductor devices or integrated circuits are considered as "technology". |
3D004
"Software" specially designed for the "development" of equipment specified in 3A003.
3D101
"Software" specially designed or modified for the "use" of equipment specified in 3A101.b.
3D225
"Software" specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225.
3E
Technology
3E001
"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 3A, 3B or 3C;
Note 1: |
3E001 does not control "technology" for the "production" of equipment or components specified in 3A003. |
Note 2: |
3E001 does not control "technology" for the "development" or "production" of integrated circuits specified in 3A001.a.3. to 3A001.a.12., having all of the following:
|
3E002
"Technology" according to the General Technology Note, other than that specified in 3E001,for the "development" or "production" of a "microprocessor microcircuit", "microcomputer microcircuit" or microcontroller microcircuit core, having an arithmetic logic unit with an access width of 32 bits or more and any of the following features or characteristics:
a. |
A 'vector processor unit' designed to perform more than two calculations on floating-point vectors (one-dimensional arrays of 32-bit or larger numbers) simultaneously; Technical Note: A 'vector processor unit' is a processor element with built-in instructions that perform multiple calculations on floating-point vectors (one-dimensional arrays of 32-bit or larger numbers) simultaneously, having at least one vector arithmetic logic unit and vector registers of at least 32 elements each. |
b. |
Designed to perform more than four 64-bit or larger floating-point operation results per cycle; or |
c. |
Designed to perform more than eight 16-bit fixed-point multiply-accumulate results per cycle (e.g., digital manipulation of analogue information that has been previously converted into digital form, also known as digital "signal processing"). |
Note 1: |
3E002 does not control "technology" for multimedia extensions. |
Note 2: |
3E002 does not control "technology" for the "development" or "production" of micro-processor cores, having all of the following:
|
Note 3: |
3E002 includes "technology" for digital signal processors and digital array processors. |
3E003
Other "technology" for the "development" or "production" of the following:
a. |
Vacuum microelectronic devices; |
b. |
Hetero-structure semiconductor electronic devices such as high electron mobility transistors (HEMT), hetero-bipolar transistors (HBT), quantum well and super lattice devices;
|
c. |
"Superconductive" electronic devices; |
d. |
Substrates of films of diamond for electronic components. |
e. |
Substrates of silicon-on-insulator (SOI) for integrated circuits in which the insulator is silicon dioxide; |
f. |
Substrates of silicon carbide for electronic components; |
g. |
Electronic vacuum tubes operating at frequencies of 31,8 GHz or higher. |
3E101
"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 3A001.a.1. or 2., 3A101, 3A102 or 3D101.
3E102
"Technology" according to the General Technology Note for the "development" of "software"specified in 3D101.
3E201
"Technology" according to the General Technology Note for the "use" of equipment specified in 3A001.e.2., 3A001.e.3., 3A001.g., 3A201, 3A225 to 3A234.
3E225
"Technology", in the form of codes or keys, to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225.
CATEGORY 4 — COMPUTERS
Note 1: |
Computers, related equipment and "software" performing telecommunications or "local area network" functions must also be evaluated against the performance characteristics of Category 5, Part 1 (Telecommunications). |
Note 2: |
Control units which directly interconnect the buses or channels of central processing units, "main storage" or disk controllers are not regarded as telecommunications equipment described in Category 5, Part 1 (Telecommunications).
|
4A
Systems, Equipment and Components
4A001
Electronic computers and related equipment, having any of the following and "electronic assemblies" and specially designed components therefor:
N.B.: |
SEE ALSO 4A101. |
a. |
Specially designed to have any of the following:
|
b. |
Not used. |
4A003
"Digital computers", "electronic assemblies", and related equipment therefor, as follows and specially designed components therefor:
Note 1: |
4A003 includes the following:
|
Note 2: |
The control status of the "digital computers" and related equipment described in 4A003 is determined by the control status of other equipment or systems provided:
|
a. |
Not used; |
b. |
"Digital computers" having an "Adjusted Peak Performance" ("APP") exceeding 12,5 Weighted TeraFLOPS (WT); |
c. |
"Electronic assemblies" specially designed or modified for enhancing performance by aggregation of processors so that the "APP" of the aggregation exceeds the limit specified in 4A003.b.;
|
d. |
Not used; |
e. |
Not used;
|
f. |
Not used; |
g. |
Equipment specially designed for aggregating the performance of "digital computers" by providing external interconnections which allows communications at unidirectional data rates exceeding 2,0 Gbyte/s per link.
|
4A004
Computers as follows and specially designed related equipment, "electronic assemblies" and components therefor:
a. |
"Systolic array computers"; |
b. |
"Neural computers"; |
c. |
"Optical computers". |
4A005
Systems, equipment, and components therefor, specially designed or modified for the generation, operation or delivery of, or communication with, "intrusion software".
4A101
Analogue computers, "digital computers" or digital differential analysers, other than those specified in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
4A102
"Hybrid computers" specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Note: |
This control only applies when the equipment is supplied with "software" specified in 7D103 or 9D103. |
4B
Test, Inspection and Production Equipment
None.
4C
Materials
None.
4D
Software
Note: |
The control status of "software" for equipment described in other Categories is dealt with in the appropriate Category. |
4D001
"Software" as follows:
a. |
"Software" specially designed or modified for the "development" or "production" of equipment or "software" specified in 4A001 to 4A004, or 4D. |
b. |
"Software", other than that specified in 4D001.a., specially designed or modified for the "development" or "production" of equipment as follows:
|
4D002
Not used
4D003
Not used.
4D004
"Software" specially designed or modified for the generation, operation or delivery of, or communication with, "intrusion software".
4E
Technology
4E001
a. |
"Technology" according to the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 4A or 4D. |
b. |
"Technology", other than that specified in 4E001.a., specially designed or modified for the "development" or "production" of equipment as follows:
|
c. |
"Technology" for the "development" of "intrusion software". |
TECHNICAL NOTE ON "ADJUSTED PEAK PERFORMANCE" ("APP")
"APP" is an adjusted peak rate at which "digital computers" perform 64-bit or larger floating point additions and multiplications.
"APP" is expressed in Weighted TeraFLOPS (WT), in units of 1012 adjusted floating point operations per second
Abbreviations used in this Technical Note
n |
number of processors in the "digital computer" |
i |
processor number (i,…n) |
ti |
processor cycle time (ti = 1/Fi) |
Fi |
processor frequency |
Ri |
peak floating point calculating rate |
Wi |
architecture adjustment factor |
Outline of "APP" calculation method
1. |
For each processor i, determine the peak number of 64-bit or larger floating point operations, FPOi, performed per cycle for each processor in the "digital computer".
|
2. |
Calculate the floating point rate R for each processor Ri = FPOi/ti. |
3. |
Calculate "APP" as "APP" = W1 × R1 + W2 × R2 + … + Wn × Rn. |
4. |
For 'vector processors', Wi = 0,9. For non-'vector processors', Wi = 0,3. |
Note 1 |
For processors that perform compound operations in a cycle, such as addition and multiplication, each operation is counted. |
Note 2 |
For a pipelined processor the effective calculating rate R is the faster of the pipelined rate, once the pipeline is full, or the non-pipelined rate. |
Note 3 |
The calculating rate R of each contributing processor is to be calculated at its maximum value theoretically possible before the "APP" of the combination is derived. Simultaneous operations are assumed to exist when the computer manufacturer claims concurrent, parallel, or simultaneous operation or execution in a manual or brochure for the computer. |
Note 4 |
Do not include processors that are limited to input/output and peripheral functions (e.g., disk drive, communication and video display) when calculating "APP". |
Note 5 |
"APP" values are not to be calculated for processor combinations (inter)connected by "Local Area Networks", Wide Area Networks, I/O shared connections/devices, I/O controllers and any communication interconnection implemented by "software". |
Note 6 |
"APP" values must be calculated for processor combinations containing processors specially designed to enhance performance by aggregation, operating simultaneously and sharing memory;
Technical Note:
|
Note 7 |
A 'vector processor' is defined as a processor with built-in instructions that perform multiple calculations on floating-point vectors (one-dimensional arrays of 64-bit or larger numbers) simultaneously, having at least 2 vector functional units and at least 8 vector registers of at least 64 elements each. |
CATEGORY 5 — TELECOMMUNICATIONS AND "INFORMATION SECURITY"
Part 1 — TELECOMMUNICATIONS
Note 1: |
The control status of components, test and "production" equipment and "software" therefor which are specially designed for telecommunications equipment or systems is determined in Category 5, Part 1.
|
Note 2: |
"Digital computers", related equipment or "software", when essential for the operation and support of telecommunications equipment described in this Category, are regarded as specially designed components, provided they are the standard models customarily supplied by the manufacturer. This includes operation, administration, maintenance, engineering or billing computer systems. |
5A1
Systems, Equipment and Components
5A001
Telecommunications systems, equipment, components and accessories as follows:
a. |
Any type of telecommunications equipment having any of the following characteristics, functions or features:
|
b. |
Telecommunication systems and equipment, and specially designed components and accessories therefor, having any of the following characteristics, functions or features:
|
c. |
Optical fibres of more than 500 m in length and specified by the manufacturer as being capable of withstanding a 'proof test' tensile stress of 2 × 109 N/m2 or more;
Technical Note: 'Proof Test': on-line or off-line production screen testing that dynamically applies a prescribed tensile stress over a 0,5 to 3 m length of fibre at a running rate of 2 to 5 m/s while passing between capstans approximately 150 mm in diameter. The ambient temperature is a nominal 293 K (20 °C) and relative humidity 40 %. Equivalent national standards may be used for executing the proof test. |
d. |
"Electronically steerable phased array antennae" as follows:
|
e. |
Radio direction finding equipment operating at frequencies above 30 MHz and having all of the following, and specially designed components therefor:
|
f. |
Mobile telecommunications interception or jamming equipment, and monitoring equipment therefor, as follows, and specially designed components therefor:
|
g. |
Passive Coherent Location (PCL) systems or equipment, specially designed for detecting and tracking moving objects by measuring reflections of ambient radio frequency emissions, supplied by non-radar transmitters; Technical Note: Non-radar transmitters may include commercial radio, television or cellular telecommunications base stations.
|
h. |
Counter Improvised Explosive Device (IED) equipment and related equipment, as follows:
|
i. |
Not used; |
j. |
Internet Protocol (IP) network communications surveillance systems or equipment, and specially designed components therefor, having all of the following:
Technical Note: 'Hard selectors' means data or set of data, related to an individual (e.g., family name, given name, e-mail, street address, phone number or group affiliations). |
5A101
Telemetry and telecontrol equipment, including ground equipment, designed or modified for 'missiles'.
Technical Note:
In 5A101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Note: |
5A101 does not control:
|
5B1
Test, Inspection and Production Equipment
5B001
Telecommunications test, inspection and production equipment, components and accessories, as follows:
a. |
Equipment and specially designed components or accessories therefor, specially designed for the "development" or "production" of equipment, functions or features, specified in 5A001;
|
b. |
Equipment and specially designed components or accessories therefor, specially designed for the "development" of any of the following telecommunication transmission or switching equipment:
|
5C1
Materials
None
5D1
Software
5D001
"Software" as follows:
a. |
"Software" specially designed or modified for the "development", "production" or "use" of equipment, functions or features, specified in 5A001; |
b. |
Not used; |
c. |
Specific "software" specially designed or modified to provide characteristics, functions or features of equipment, specified in 5A001 or 5B001; |
d. |
"Software" specially designed or modified for the "development" of any of the following telecommunication transmission or switching equipment:
|
5D101
"Software" specially designed or modified for the "use" of equipment specified in 5A101.
5E1
Technology
5E001
"Technology" as follows:
a. |
"Technology" according to the General Technology Note for the "development", "production" or "use" (excluding operation) of equipment, functions or features specified in 5A001 or "software" specified in 5D001.a.; |
b. |
Specific "technology" as follows:
|
c. |
"Technology" according to the General Technology Note for the "development" or "production" of any of the following:
|
d. |
"Technology" according to the General Technology Note for the "development" or "production" of Microwave Monolithic Integrated Circuit (MMIC) power amplifiers specially designed for telecommunications and that are any of the following: Technical Note: For purposes of 5E001.d., the parameter peak saturated power output may also be referred to on product data sheets as output power, saturated power output, maximum power output, peak power output, or peak envelope power output.
|
e. |
"Technology" according to the General Technology Note for the "development" or "production" of electronic devices and circuits, specially designed for telecommunications and containing components manufactured from "superconductive" materials, specially designed for operation at temperatures below the "critical temperature" of at least one of the "superconductive" constituents and having any of the following:
|
5E101
"Technology" according to the General Technology Note for the "development", "production" or "use" of equipment specified in 5A101.
Part 2 — "INFORMATION SECURITY"
Note 1: |
Not used. |
Note 2: |
Category 5 — Part 2 does not control products when accompanying their user for the user's personal use. |
Note 3: |
Cryptography Note 5A002, 5A003, 5A004 and 5D002 do not control items as follows:
Note to the Cryptography Note:
|
Note 4: |
Category 5 — Part 2 does not control items incorporating or using "cryptography" and meeting all of the following:
|
5A2
Systems, Equipment and Components
5A002
"Information security" systems, equipment and components, as follows:
a. |
Systems, equipment and components for cryptographic "information security", as follows,
|
b. |
Designed or modified to enable, by means of "cryptographic activation" an item to achieve or exceed the controlled performance levels for functionality specified in 5A002.a. that would not otherwise be enabled. |
c. |
Designed or modified to use or perform "quantum cryptography"; Technical Note: "Quantum cryptography" is also known as Quantum Key Distribution (QKD). |
d. |
Designed or modified to use cryptographic techniques to generate channelising codes, scrambling codes or network identification codes, for systems using ultra-wideband modulation techniques and having any of the following:
|
e. |
Designed or modified to use cryptographic techniques to generate the spreading code for "spread spectrum" systems, other than those specified in 5A002.d., including the hopping code for "frequency hopping" systems. |
5A003
Systems, equipment and components, for non-cryptographic "information security", as follows:
a. |
Communications cable systems designed or modified using mechanical, electrical or electronic means to detect surreptitious intrusion;
|
b. |
Specially designed or modified to reduce the compromising emanations of information-bearing signals beyond what is necessary for health, safety or electromagnetic interference standards; |
5A004
Systems, equipment and components for defeating, weakening or bypassing "information security", as follows:
a. |
Designed or modified to perform 'cryptanalytic functions';
Technical Note 'Cryptanalytic functions' are functions designed to defeat cryptographic mechanisms in order to derive confidential variables or sensitive data, including clear text, passwords or cryptographic keys. |
5B2
Test, Inspection and Production Equipment
5B002
"Information security" test, inspection and "production" equipment, as follows:
a. |
Equipment specially designed for the "development" or "production" of equipment specified in 5A002, 5A003, 5A004 or 5B002.b.; |
b. |
Measuring equipment specially designed to evaluate and validate the "information security" functions of the equipment specified in 5A002, 5A003 or 5A004, or of "software" specified in 5D002.a. or 5D002.c. |
5C2
Materials
None.
5D2
Software
5D002
"Software" as follows:
a. |
"Software" specially designed or modified for the "development", "production" or "use" of equipment specified in 5A002, 5A003 or 5A004, or of "software" specified in 5D002.c.; |
b. |
"Software" specially designed or modified to support "technology" specified in 5E002; |
c. |
Specific "software", as follows:
|
d. |
"Software" designed or modified to enable, by means of "cryptographic activation", an item to meet the criteria for functionality specified by 5A002.a., that would not otherwise be met. |
5E2
Technology
5E002
"Technology" as follows:
a. |
"Technology" according to the General Technology Note for the "development", "production" or "use" of equipment specified in 5A002, 5A003, 5A004 or 5B002, or of "software" specified in 5D002.a. or 5D002.c. |
b. |
"Technology" to enable, by means of "cryptographic activation", an item to meet the criteria for functionality specified by 5A002.a., that would not otherwise be met. |
Note: |
5E002 includes "information security" technical data resulting from procedures carried out to evaluate or determine the implementation of functions, features or techniques specified in Category 5-Part 2. |
CATEGORY 6 — SENSORS AND LASERS
6A
Systems, Equipment and Components
6A001
Acoustic systems, equipment and components, as follows:
a. |
Marine acoustic systems, equipment and specially designed components therefor, as follows:
|
b. |
Correlation-velocity and Doppler-velocity sonar log equipment, designed to measure the horizontal speed of the equipment carrier relative to the sea bed, as follows:
|
c. |
Not used. |
6A002
Optical sensors or equipment and components therefor, as follows:
N.B.: |
SEE ALSO 6A102. |
a. |
Optical detectors as follows:
|
b. |
"Monospectral imaging sensors" and "multispectral imaging sensors", designed for remote sensing applications and having any of the following:
|
c. |
'Direct view' imaging equipment incorporating any of the following:
Technical Note: 'Direct view' refers to imaging equipment that presents a visual image to a human observer without converting the image into an electronic signal for television display, and that cannot record or store the image photographically, electronically or by any other means.
|
d. |
Special support components for optical sensors, as follows:
|
e. |
Not used. |
6A003
Cameras, systems or equipment, and components therefor, as follows:
N.B.: |
SEE ALSO 6A203. |
a. |
Instrumentation cameras and specially designed components therefor, as follows:
|
b. |
Imaging cameras as follows:
|
6A004
Optical equipment and components, as follows:
a. |
Optical mirrors (reflectors) as follows: Technical Note: For the purpose of 6A004.a., Laser Induced Damage Threshold (LIDT) is measured according to ISO 21254-1:2011.
|
b. |
Optical components made from zinc selenide (ZnSe) or zinc sulphide (ZnS) with transmission in the wavelength range exceeding 3 000 nm but not exceeding 25 000 nm and having any of the following:
|
c. |
"Space-qualified" components for optical systems, as follows:
|
d. |
Optical control equipment as follows:
|
e. |
'Aspheric optical elements' having all of the following:
Technical Notes:
|
6A005
"Lasers", other than those specified in 0B001.g.5. or 0B001.h.6., components and optical equipment, as follows:
N.B.: |
SEE ALSO 6A205. |
Note 1: |
Pulsed "lasers" include those that run in a continuous wave (CW) mode with pulses superimposed. |
Note 2: |
Excimer, semiconductor, chemical, CO, CO2, and 'non-repetitive pulsed' Nd:glass "lasers" are only specified in 6A005.d.
Technical Note: 'Non-repetitive pulsed' refers to "lasers" that produce either a single output pulse or that have a time interval between pulses exceeding one minute. |
Note 3: |
6A005 includes fibre "lasers". |
Note 4: |
The control status of "lasers" incorporating frequency conversion (i.e., wavelength change) by means other than one "laser" pumping another "laser" is determined by applying the control parameters for both the output of the source "laser" and the frequency-converted optical output. |
Note 5: |
6A005 does not control "lasers" as follows:
|
Technical Note:
In 6A005 'Wall-plug efficiency' is defined as the ratio of "laser" output power (or "average output power") to total electrical input power required to operate the "laser", including the power supply/conditioning and thermal conditioning/heat exchanger.
a. |
Non-"tunable" continuous wave "(CW) lasers" having any of the following:
|
b. |
Non-"tunable" "pulsed lasers" having any of the following:
|
c. |
"Tunable" "lasers" having any of the following:
|
d. |
Other "lasers", not specified in 6A005.a., 6A005.b. or 6A005.c. as follows:
|
e. |
Components as follows:
|
f. |
Optical equipment as follows:
|
g. |
'Laser acoustic detection equipment' having all of the following:
Technical Note: 'Laser acoustic detection equipment' is sometimes referred to as a "Laser" Microphone or Particle Flow Detection Microphone. |
6A006
"Magnetometers", "magnetic gradiometers", "intrinsic magnetic gradiometers", underwater electric field sensors, "compensation systems", and specially designed components therefor, as follows:
N.B.: |
SEE ALSO 7A103.d. |
Note: |
6A006 does not control instruments specially designed for fishery applications or biomagnetic measurements for medical diagnostics. |
a. |
"Magnetometers" and subsystems as follows:
|
b. |
Underwater electric field sensors having a 'sensitivity' lower (better) than 8 nanovolt per metre per square root Hz when measured at 1 Hz; |
c. |
"Magnetic gradiometers" as follows:
|
d. |
"Compensation systems" for magnetic or underwater electric field sensors resulting in a performance equal to or better than the specified parameters of 6A006.a., 6A006.b. or 6A006.c.; |
e. |
Underwater electromagnetic receivers incorporating magnetic field sensors specified by 6A006.a. or underwater electric field sensors specified by 6A006.b. |
Technical Note:
For the purposes of 6A006., 'sensitivity' (noise level) is the root mean square of the device-limited noise floor which is the lowest signal that can be measured.
6A007
Gravity meters (gravimeters) and gravity gradiometers, as follows:
N.B.: |
SEE ALSO 6A107. |
a. |
Gravity meters designed or modified for ground use and having a static "accuracy" of less (better) than 10 μGal;
|
b. |
Gravity meters designed for mobile platforms and having all of the following:
Technical Note: For the purposes of 6A007.b., 'time-to-steady-state registration' (also referred to as the gravimeter's response time) is the time over which the disturbing effects of platform induced accelerations (high frequency noise) are reduced. |
c. |
Gravity gradiometers. |
6A008
Radar systems, equipment and assemblies, having any of the following, and specially designed components therefor:
N.B.: |
SEE ALSO 6A108. |
Note: |
6A008 does not control:
|
a. |
Operating at frequencies from 40 GHz to 230 GHz and having any of the following:
|
b. |
A tunable bandwidth exceeding ± 6,25 % of the 'centre operating frequency'; Technical Note: The 'centre operating frequency' equals one half of the sum of the highest plus the lowest specified operating frequencies. |
c. |
Capable of operating simultaneously on more than two carrier frequencies; |
d. |
Capable of operating in synthetic aperture (SAR), inverse synthetic aperture (ISAR) radar mode, or sidelooking airborne (SLAR) radar mode; |
e. |
Incorporating electronically steerable array antennae; |
f. |
Capable of heightfinding non-cooperative targets; |
g. |
Specially designed for airborne (balloon or airframe mounted) operation and having Doppler "signal processing" for the detection of moving targets; |
h. |
Employing processing of radar signals and using any of the following:
|
i. |
Providing ground-based operation with a maximum "instrumented range" exceeding 185 km;
|
j. |
Being "laser" radar or Light Detection and Ranging (LIDAR) equipment and having any of the following:
|
k. |
Having "signal processing" sub-systems using "pulse compression" and having any of the following:
|
l. |
Having data processing sub-systems and having any of the following:
|
Technical Notes:
1. |
For the purposes of 6A008, 'marine radar' is a radar that is used to navigate safely at sea, inland waterways or near-shore environments. |
2. |
For the purposes of 6A008, 'vessel traffic service' is a vessel traffic monitoring and control service similar to air traffic control for "aircraft". |
6A102
Radiation hardened 'detectors', other than those specified in 6A002, specially designed or modified for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects) and usable for "missiles", designed or rated to withstand radiation levels which meet or exceed a total irradiation dose of 5 × 105 rads (silicon).
Technical Note:
In 6A102, a 'detector' is defined as a mechanical, electrical, optical or chemical device that automatically identifies and records, or registers a stimulus such as an environmental change in pressure or temperature, an electrical or electromagnetic signal or radiation from a radioactive material. This includes devices that sense by one time operation or failure.
6A107
Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows:
a. |
Gravity meters, other than those specified in 6A007.b, designed or modified for airborne or marine use, and having a static or operational accuracy equal to or less (better) than 0,7 milligal (mgal), and having a time-to-steady-state registration of two minutes or less; |
b. |
Specially designed components for gravity meters specified in 6A007.b or 6A107.a. and gravity gradiometers specified in 6A007.c. |
6A108
Radar systems and tracking systems, other than those specified in entry 6A008, as follows:
a. |
Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
|
b. |
Precision tracking systems, usable for 'missiles', as follows:
Technical Note: In 6A108.b. 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
6A202
Photomultiplier tubes having both of the following characteristics:
a. |
Photocathode area of greater than 20 cm2; and |
b. |
Anode pulse rise time of less than 1 ns. |
6A203
Cameras and components, other than those specified in 6A003, as follows:
N.B. 1: |
"Software" specially designed to enhance or release the performance of a camera or imaging device to meet the characteristics of 6A203.a., 6A203.b. or 6A203.c. is specified in 6D203. |
N.B. 2: |
"Technology" in the form of codes or keys to enhance or release the performance of a camera or imaging device to meet the characteristics of 6A203.a., 6A203.b. or 6A203.c is specified in 6E203. |
Note: |
6A203.a. to 6A203.c. does not control cameras or imaging devices if they have hardware, "software" or "technology" constraints that limit the performance to less than that specified above, provided they meet any of the following:
|
a. |
Streak cameras, and specially designed components therefor, as follows:
|
b. |
Framing cameras, and specially designed components therefor, as follows:
Technical Note: In 6A203.b., high speed single frame cameras can be used alone to produce a single image of a dynamic event, or several such cameras can be combined in a sequentially-triggered system to produce multiple images of an event. |
c. |
Solid state or electron tube cameras, and specially designed components therefor, as follows:
|
d. |
Radiation-hardened TV cameras, or lenses therefor, specially designed or rated as radiation hardened to withstand a total radiation dose greater than 50 × 103 Gy(silicon) (5 × 106 rad (silicon)) without operational degradation. Technical Note: The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation. |
6A205
"Lasers", "laser" amplifiers and oscillators, other than those specified in 0B001.g.5., 0B001.h.6. and 6A005; as follows:
N.B.: |
For copper vapour lasers, see 6A005.b. |
a. |
Argon ion "lasers" having both of the following characteristics:
|
b. |
Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:
|
c. |
Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:
|
d. |
Pulsed carbon dioxide "lasers" having all of the following characteristics:
|
e. |
Para-hydrogen Raman shifters designed to operate at 16 μm output wavelength and at a repetition rate greater than 250 Hz; |
f. |
Neodymium-doped (other than glass) "lasers" with an output wavelength between 1 000 and 1 100 nm having either of the following:
|
g. |
Pulsed carbon monoxide lasers, other than those specified in 6A005.d.2., having all of the following:
|
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), DLIs (Doppler Laser Interferometers) and PDV (Photonic Doppler Velocimeters) also known as Het-V (Heterodyne Velocimeters). |
6A226
Pressure sensors, as follows:
a. |
Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2); |
b. |
Quartz pressure transducers for pressures greater than 10 GPa. |
6B
Test, Inspection and Production Equipment
6B004
Optical equipment as follows:
a. |
Equipment for measuring absolute reflectance to an "accuracy" of equal to or better than 0,1 % of the reflectance value; |
b. |
Equipment other than optical surface scattering measurement equipment, having an unobscured aperture of more than 10 cm, specially designed for the non-contact optical measurement of a non-planar optical surface figure (profile) to an "accuracy" of 2 nm or less (better) against the required profile. |
Note: |
6B004 does not control microscopes. |
6B007
Equipment to produce, align and calibrate land-based gravity meters with a static "accuracy" of better than 0,1 mGal.
6B008
Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor.
N.B.: |
SEE ALSO 6B108. |
6B108
Systems, other than those specified in 6B008, specially designed for radar cross section measurement usable for 'missiles' and their subsystems.
Technical Note:
In 6B108 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
6C
Materials
6C002
Optical sensor materials as follows:
a. |
Elemental tellurium (Te) of purity levels of 99,9995 % or more; |
b. |
Single crystals (including epitaxial wafers) of any of the following:
|
6C004
Optical materials as follows:
a. |
Zinc selenide (ZnSe) and zinc sulphide (ZnS) "substrate blanks", produced by the chemical vapour deposition process and having any of the following:
|
b. |
Electro-optic materials and non-linear optical materials, as follows:
|
c. |
Non-linear optical materials, other than those specified in 6C004.b., having any of the following:
|
d. |
"Substrate blanks" of silicon carbide or beryllium beryllium (Be/Be) deposited materials, exceeding 300 mm in diameter or major axis length; |
e. |
Glass, including fused silica, phosphate glass, fluorophosphate glass, zirconium fluoride (ZrF4) (CAS 7783-64-4) and hafnium fluoride (HfF4) (CAS 13709-52-9) and having all of the following:
|
f. |
Synthetically produced diamond material with an absorption of less than 10– 5 cm– 1 for wavelengths exceeding 200 nm but not exceeding 14 000 nm. |
6C005
"Laser" materials as follows:
a. |
Synthetic crystalline "laser" host material in unfinished form as follows:
|
b. |
Rare-earth-metal doped double-clad fibres having any of the following:
|
6D
Software
6D001
"Software" specially designed for the "development" or "production" of equipment specified in 6A004, 6A005, 6A008 or 6B008.
6D002
"Software" specially designed for the "use" of equipment specified in 6A002.b., 6A008 or 6B008.
6D003
Other "software" as follows:
a. |
"Software" as follows:
|
b. |
Not used; |
c. |
"Software" designed or modified for cameras incorporating "focal plane arrays" specified in 6A002.a.3.f. and designed or modified to remove a frame rate restriction and allow the camera to exceed the frame rate specified in 6A003.b.4. Note 3.a. |
d. |
"Software" specially designed to maintain the alignment and phasing of segmented mirror systems consisting of mirror segments having a diameter or major axis length equal to or larger than 1 m; |
e. |
Not used; |
f. |
"Software" as follows:
|
g. |
"Software" specially designed to correct motional influences of gravity meters or gravity gradiometers; |
h. |
"Software" as follows:
|
6D102
"Software" specially designed or modified for the "use" of goods specified in 6A108.
6D103
"Software" which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for 'missiles'.
Technical Note:
In 6D103 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
6D203
"Software" specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203.a. to 6A203.c.
6E
Technology
6E001
"Technology" according to the General Technology Note for the "development" of equipment, materials or "software" specified in 6A, 6B, 6C or 6D.
6E002
"Technology" according to the General Technology Note for the "production" of equipment or materials specified in 6A, 6B or 6C.
6E003
Other "technology" as follows:
a. |
"Technology" as follows:
|
b. |
"Technology" "required" for the "development", "production" or "use" of specially designed diagnostic instruments or targets in test facilities for "SHPL" testing or testing or evaluation of materials irradiated by "SHPL" beams; |
6E101
"Technology" according to the General Technology Note for the "use" of equipment or "software" specified in 6A002, 6A007.b. and c., 6A008, 6A102, 6A107, 6A108, 6B108, 6D102 or 6D103.
Note: |
6E101 only controls "technology" for items specified in 6A002, 6A007 and 6A008 if the items were designed for airborne applications and are usable in "missiles". |
6E201
"Technology" according to the General Technology Note for the "use" of equipment specified in 6A003, 6A005.a.2., 6A005.b.2., 6A005.b.3., 6A005.b.4., 6A005.b.6., 6A005.c.2., 6A005.d.3.c., 6A005.d.4.c., 6A202, 6A203, 6A205, 6A225 or 6A226.
Note: |
6E201 only controls "technology" for cameras specified in 6A003 if the cameras are also specified by any of the control parameters of 6A203. |
6E203
"Technology", in the form of codes or keys, to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203a. to 6A203.c.
CATEGORY 7 — NAVIGATION AND AVIONICS
7A
Systems, Equipment and Components
N.B.: |
For automatic pilots for underwater vehicles, see Category 8. For radar, see Category 6. |
7A001
Accelerometers as follows and specially designed components therefor:
N.B.: |
SEE ALSO 7A101. |
N.B.: |
For angular or rotational accelerometers, see 7A001.b. |
a. |
Linear accelerometers having any of the following:
|
b. |
Angular or rotational accelerometers, specified to function at linear acceleration levels exceeding 100 g. |
7A002
Gyros or angular rate sensors, having any of the following and specially designed components therefor:
N.B.: |
SEE ALSO 7A102. |
N.B.: |
For angular or rotational accelerometers, see 7A001.b. |
a. |
Specified to function at linear acceleration levels less than or equal to 100 g and having any of the following:
|
b. |
Specified to function at linear acceleration levels exceeding 100 g. |
7A003
'Inertial measurement equipment or systems', having any of the following:
N.B.: |
SEE ALSO 7A103. |
Note 1: |
'Inertial measurement equipment or systems' incorporate accelerometers or gyroscopes to measure changes in velocity and orientation in order to determine or maintain heading or position without requiring an external reference once aligned. 'Inertial measurement equipment or systems' include:
|
Note 2: |
7A003 does not control 'inertial measurement equipment or systems' which are certified for use on "civil aircraft" by civil aviation authorities of one or more EU Member States or Wassenaar Arrangement Participating States. |
Technical Note:
'Positional aiding references' independently provide position, and include:
a. |
Global Navigation Satellite Systems (GNSS); |
b. |
"Data-Based Referenced Navigation" ("DBRN"). |
a. |
Designed for "aircraft", land vehicles or vessels, providing position without the use of 'positional aiding references', and having any of the following "accuracies" subsequent to normal alignment:
Technical Note: The performance parameters in 7A003.a.1., 7A003.a.2. and 7A003.a.3. typically apply to 'inertial measurement equipment or systems' designed for "aircraft", vehicles and vessels, respectively. These parameters result from the utilisation of specialised non-positional aiding references (e.g., altimeter, odometer, velocity log). As a consequence, the specified performance values cannot be readily converted between these parameters. Equipment designed for multiple platforms are evaluated against each applicable entry 7A003.a.1., 7A003.a.2., or 7A003.a.3. |
b. |
Designed for "aircraft", land vehicles or vessels, with an embedded 'positional aiding reference' and providing position after loss of all 'positional aiding references' for a period of up to 4 minutes, having an "accuracy" of less (better) than 10 meters "CEP"; Technical Note: 7A003.b. refers to systems in which 'inertial measurement equipment or systems' and other independent 'positional aiding references' are built into a single unit (i.e., embedded) in order to achieve improved performance. |
c. |
Designed for "aircraft", land vehicles or vessels, providing heading or True North determination and having any of the following:
|
d. |
Providing acceleration measurements or angular rate measurements, in more than one dimension, and having any of the following:
|
7A004
'Star trackers' and components therefor, as follows:
N.B.: |
SEE ALSO 7A104. |
a. |
'Star trackers' with a specified azimuth "accuracy" of equal to or less (better) than 20 seconds of arc throughout the specified lifetime of the equipment; |
b. |
Components specially designed for equipment specified in 7A004.a. as follows:
|
Technical Note:
'Star trackers' are also referred to as stellar attitude sensors or gyro-astro compasses.
7A005
Global Navigation Satellite Systems (GNSS) receiving equipment having any of the following and specially designed components therefor:
N.B.: |
SEE ALSO 7A105. |
N.B.: |
For equipment specially designed for military use, see Military Goods Controls. |
a. |
Employing a decryption algorithm specially designed or modified for government use to access the ranging code for position and time; or |
b. |
Employing 'adaptive antenna systems'.
Technical Note: For the purposes of 7A005.b 'adaptive antenna systems' dynamically generate one or more spatial nulls in an antenna array pattern by signal processing in the time domain or frequency domain. |
7A006
Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive and having any of the following:
N.B.: |
SEE ALSO 7A106. |
a. |
"Power management"; or |
b. |
Using phase shift key modulation. |
7A008
Underwater sonar navigation systems using doppler velocity or correlation velocity logs integrated with a heading source and having a positioning "accuracy" of equal to or less (better) than 3 % of distance travelled "Circular Error Probable" ("CEP") and specially designed components therefor.
Note: |
7A008 does not control systems specially designed for installation on surface vessels or systems requiring acoustic beacons or buoys to provide positioning data. |
N.B.: |
See 6A001.a. for acoustic systems, and 6A001.b. for correlation-velocity and Doppler-velocity sonar log equipment.
See 8A002 for other marine systems. |
7A101
Linear accelerometers, other than those specified in 7A001, designed for use in inertial navigation systems or in guidance systems of all types, usable in 'missiles', having all the following characteristics, and specially designed components therefor:
a. |
A "bias" "repeatability" of less (better) than 1 250 micro g; and |
b. |
A "scale factor" "repeatability" of less (better) than 1 250 ppm; |
Note: |
7A101 does not control accelerometers specially designed and developed as Measurement While Drilling (MWD) Sensors for use in downhole well service operations. |
Technical Notes:
1. |
In 7A101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km; |
2. |
In 7A101 the measurement of "bias" and "scale factor" refers to one sigma standard deviation with respect to a fixed calibration over a period of one year; |
7A102
All types of gyros, other than those specified in 7A002, usable in 'missiles', with a rated "drift rate" 'stability' of less than 0,5° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor.
Technical Notes:
1. |
In 7A102 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
2. |
In 7A102 'stability' is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition (IEEE STD 528-2001 paragraph 2,247). |
7A103
Instrumentation, navigation equipment and systems, other than those specified in 7A003, as follows; and specially designed components therefor:
a. |
Inertial or other equipment, using accelerometers or gyros as follows, and systems incorporating such equipment:
|
b. |
Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in 'missiles'; |
c. |
'Integrated navigation systems', designed or modified for 'missiles' and capable of providing a navigational accuracy of 200 m Circle of Equal Probability or less; Technical Note: An 'integrated navigation system' typically incorporates the following components:
|
d. |
Three axis magnetic heading sensors, designed or modified to be integrated with flight control and navigation systems, other than those specified in 6A006, having all the following characteristics, and specially designed components therefor;
|
Technical Note:
In 7A103 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
7A104
Gyro-astro compasses and other devices, other than those specified in 7A004, which derive position or orientation by means of automatically tracking celestial bodies or satellites and specially designed components therefor.
7A105
Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS, or Galileo), other than those specified in 7A005, having any of the following characteristics, and specially designed components therefor:
a. |
Designed or modified for use in space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a; or |
b. |
Designed or modified for airborne applications and having any of the following:
|
7A106
Altimeters, other than those specified in 7A006, of radar or laser radar type, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
7A115
Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Note: |
7A115 includes sensors for the following equipment:
|
7A116
Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in 9A004 sounding rockets specified in 9A104 or "missiles".
a. |
Pneumatic, hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems (including fly-by-wire and fly-by-light systems); |
b. |
Attitude control equipment; |
c. |
Flight control servo valves designed or modified for the systems specified in 7A116.a. or 7A116.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz. |
7A117
"Guidance sets", usable in "missiles" capable of achieving system accuracy of 3,33 % or less of the range (e.g., a "CEP" of 10 km or less at a range of 300 km).
7B
Test, Inspection and Production Equipment
7B001
Test, calibration or alignment equipment, specially designed for equipment specified in 7A.
Note: |
7B001 does not control test, calibration or alignment equipment for 'Maintenance Level I' or 'Maintenance Level II'. |
Technical Notes:
1. 'Maintenance Level I'
The failure of an inertial navigation unit is detected on the "aircraft" by indications from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of the failure may be localised at the level of the malfunctioning Line Replaceable Unit (LRU). The operator then removes the LRU and replaces it with a spare.
2. 'Maintenance Level II'
The defective LRU is sent to the maintenance workshop (the manufacturer's or that of the operator responsible for level II maintenance). At the maintenance workshop, the malfunctioning LRU is tested by various appropriate means to verify and localise the defective Shop Replaceable Assembly (SRA) module responsible for the failure. This SRA is removed and replaced by an operative spare. The defective SRA (or possibly the complete LRU) is then shipped to the manufacturer. 'Maintenance Level II' does not include the disassembly or repair of controlled accelerometers or gyro sensors.
7B002
Equipment specially designed to characterize mirrors for ring "laser" gyros, as follows:
N.B.: |
SEE ALSO 7B102. |
a. |
Scatterometers having a measurement "accuracy" of 10 ppm or less (better); |
b. |
Profilometers having a measurement "accuracy" of 0,5 nm (5 angstrom) or less (better). |
7B003
Equipment specially designed for the "production" of equipment specified in 7A.
Note: |
7B003 includes:
|
7B102
Reflectometers specially designed to characterise mirrors, for "laser" gyros, having a measurement accuracy of 50 ppm or less (better).
7B103
"Production facilities" and "production equipment" as follows:
a. |
"Production facilities" specially designed for equipment specified in 7A117; |
b. |
"Production equipment", and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A. |
7C
Materials
None.
7D
Software
7D001
"Software" specially designed or modified for the "development" or "production" of equipment specified in 7A. or 7B.
7D002
"Source code" for the operation or maintenance of any inertial navigation equipment, including inertial equipment not specified in 7A003 or 7A004, or Attitude and Heading Reference Systems ('AHRS').
Note: |
7D002 does not control "source code" for the "use" of gimballed 'AHRS'. |
Technical Note:
'AHRS' generally differ from Inertial Navigation Systems (INS) in that an 'AHRS' provides attitude and heading information and normally does not provide the acceleration, velocity and position information associated with an INS.
7D003
a. |
"Software" specially designed or modified to improve the operational performance or reduce the navigational error of systems to the levels specified in 7A003, 7A004 or 7A008; |
b. |
"Source code" for hybrid integrated systems which improves the operational performance or reduces the navigational error of systems to the level specified in 7A003 or 7A008 by continuously combining heading data with any of the following:
|
c. |
Not used; |
d. |
Not used; |
e. |
Computer-Aided-Design (CAD) "software" specially designed for the "development" of "active flight control systems", helicopter multi-axis fly-by-wire or fly-by-light controllers or helicopter "circulation controlled anti-torque or circulation-controlled direction control systems", whose "technology" is specified in 7E004.b., 7E004.c.1. or 7E004.c.2. |
7D004
"Source code" incorporating "development" "technology" specified in 7E004.a.1. to 7E004.a.6. or 7E004.b.,for any of the following:
a. |
Digital flight management systems for "total control of flight"; |
b. |
Integrated propulsion and flight control systems; |
c. |
"Fly-by-wire systems" or "fly-by-light systems"; |
d. |
Fault-tolerant or self-reconfiguring "active flight control systems"; |
e. |
Not used; |
f. |
Air data systems based on surface static data; or |
g. |
Three dimensional displays. |
Note: |
7D004. does not control "source code" associated with common computer elements and utilities (e.g., input signal acquisition, output signal transmission, computer program and data loading, built-in test, task scheduling mechanisms) not providing a specific flight control system function. |
7D005
"Software" specially designed to decrypt Global Navigation Satellite Systems (GNSS) ranging code designed for government use.
7D101
"Software" specially designed or modified for the "use" of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7B003, 7B102 or 7B103.
7D102
Integration "software" as follows:
a. |
Integration "software" for the equipment specified in 7A103.b.; |
b. |
Integration "software" specially designed for the equipment specified in 7A003 or 7A103.a. |
c. |
Integration "software" designed or modified for the equipment specified in 7A103.c. |
Note: |
A common form of integration "software" employs Kalman filtering. |
7D103
"Software" specially designed for modelling or simulation of the "guidance sets" specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Note: |
"Software" specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102. |
7D104
"Software" specially designed or modified for the operation or maintenance of "guidance sets" specified in 7A117.
Note: |
7D104 includes ″software″, specially designed or modified to enhance the performance of ″guidance sets″ to achieve or exceed the accuracy specified in 7A117. |
7E
Technology
7E001
"Technology" according to the General Technology Note for the "development" of equipment or "software", specified in 7A, 7B, 7D001, 7D002, 7D003, 7D005 and 7D101 to 7D103.
Note: |
7E001 includes key management "technology" exclusively for equipment specified in 7A005.a. |
7E002
"Technology" according to the General Technology Note for the "production" of equipment specified in 7A or 7B.
7E003
"Technology" according to the General Technology Note for the repair, refurbishing or overhaul of equipment specified in 7A001 to 7A004.
Note: |
7E003 does not control maintenance "technology" directly associated with calibration, removal or replacement of damaged or unserviceable LRUs and SRAs of a "civil aircraft" as described in 'Maintenance Level I' or 'Maintenance Level II'. |
N.B.: |
See Technical Notes to 7B001. |
7E004
Other "technology" as follows:
a. |
"Technology" for the "development" or "production" of any of the following:
|
b. |
"Development" "technology", as follows, for "active flight control systems" (including "fly-by-wire systems" or "fly-by-light systems"):
|
c. |
"Technology" for the "development" of helicopter systems, as follows:
|
7E101
"Technology" according to the General Technology Note for the "use" of equipment specified in 7A001 to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7B001, 7B002, 7B003, 7B102, 7B103, 7D101 to 7D103.
7E102
"Technology" for protection of avionics and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from external sources, as follows:
a. |
Design "technology" for shielding systems; |
b. |
Design "technology" for the configuration of hardened electrical circuits and subsystems; |
c. |
Design "technology" for the determination of hardening criteria of 7E102.a. and 7E102.b. |
7E104
"Technology" for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory.
CATEGORY 8 — MARINE
8A
Systems, Equipment and Components
8A001
Submersible vehicles and surface vessels, as follows:
N.B.: |
For the control status of equipment for submersible vehicles, see:
|
a. |
Manned, tethered submersible vehicles designed to operate at depths exceeding 1 000 m; |
b. |
Manned, untethered submersible vehicles having any of the following:
Technical Notes:
|
c. |
Unmanned, tethered submersible vehicles designed to operate at depths exceeding 1 000 m and having any of the following:
|
d. |
Unmanned, untethered submersible vehicles having any of the following:
|
e. |
Ocean salvage systems with a lifting capacity exceeding 5 MN for salvaging objects from depths exceeding 250 m and having any of the following:
|
f. |
Not used |
g. |
Not used |
h. |
Not used |
i. |
Not used |
8A002
Marine systems, equipment and components, as follows:
Note: |
For underwater communications systems, see Category 5, Part 1 — Telecommunications. |
a. |
Systems, equipment and components, specially designed or modified for submersible vehicles and designed to operate at depths exceeding 1 000 m, as follows:
|
b. |
Systems specially designed or modified for the automated control of the motion of submersible vehicles specified in 8A001, using navigation data, having closed loop servo-controls and having any of the following:
|
c. |
Fibre optic pressure hull penetrators; |
d. |
Underwater vision systems specially designed or modified for remote operation with an underwater vehicle, employing techniques to minimise the effects of back scatter and including range-gated illuminators or "laser" systems; |
e. |
Not used; |
f. |
Not used; |
g. |
Light systems specially designed or modified for underwater use, as follows:
|
h. |
"Robots" specially designed for underwater use, controlled by using a dedicated computer and having any of the following:
|
i. |
Remotely controlled articulated manipulators specially designed or modified for use with submersible vehicles and having any of the following:
|
j. |
Air independent power systems specially designed for underwater use, as follows:
|
k. |
Not used |
l. |
Not used |
m. |
Not used |
n. |
Not used |
o. |
Propellers, power transmission systems, power generation systems and noise reduction systems, as follows:
|
p. |
Pumpjet propulsion systems having all of the following:
|
q. |
Underwater swimming and diving equipment as follows:
|
r. |
Diver deterrent acoustic systems specially designed or modified to disrupt divers and having a sound pressure level equal to or exceeding 190 dB (reference 1 μPa at 1 m) at frequencies of 200 Hz and below.
|
8B
Test, Inspection and Production Equipment
8B001
Water tunnels having a background noise of less than 100 dB (reference 1 μPa, 1 Hz), in the frequency range from 0 to 500 Hz and designed for measuring acoustic fields generated by a hydro-flow around propulsion system models.
8C
Materials
8C001
'Syntactic foam' designed for underwater use and having all of the following:
N.B.: |
See also 8A002.a.4. |
a. |
Designed for marine depths exceeding 1 000 m; and |
b. |
A density less than 561 kg/m3. |
Technical Note:
'Syntactic foam' consists of hollow spheres of plastic or glass embedded in a resin matrix.
8D
Software
8D001
"Software" specially designed or modified for the "development", "production" or "use" of equipment or materials, specified in 8A, 8B or 8C.
8D002
Specific "software" specially designed or modified for the "development", "production", repair, overhaul or refurbishing (re-machining) of propellers specially designed for underwater noise reduction.
8E
Technology
8E001
"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials, specified in 8A, 8B or 8C.
8E002
Other "technology" as follows:
a. |
"Technology" for the "development", "production", repair, overhaul or refurbishing (re-machining) of propellers specially designed for underwater noise reduction; |
b. |
"Technology" for the overhaul or refurbishing of equipment specified in 8A001, 8A002.b., 8A002.j., 8A002.o. or 8A002.p. |
c. |
"Technology" according to the General Technology Note for the "development" or "production" of any of the following:
Technical Note: A 'small waterplane area vessel' is defined by the following formula: waterplane area at an operational design draft less than 2x (displaced volume at the operational design draft) 2/3. |
CATEGORY 9 — AEROSPACE AND PROPULSION
9A
Systems, Equipment and Components
N.B.: |
For propulsion systems designed or rated against neutron or transient ionizing radiation, see the Military Goods Controls. |
9A001
Aero gas turbine engines having any of the following:
N.B.: |
SEE ALSO 9A101. |
a. |
Incorporating any of the "technologies" specified in 9E003.a., 9E003.h. or 9E003.i.; or
|
b. |
Designed to power an "aircraft" to cruise at Mach 1 or higher, for more than thirty minutes. |
9A002
'Marine gas turbine engines' with an ISO standard continuous power rating of 24 245 kW or more and a specific fuel consumption not exceeding 0,219 kg/kWh in the power range from 35 to 100 %, and specially designed assemblies and components therefor.
Note: |
The term 'marine gas turbine engines' includes those industrial, or aero-derivative, gas turbine engines adapted for a ship's electric power generation or propulsion. |
9A003
Specially designed assemblies or components, incorporating any of the "technologies" specified in 9E003.a., 9E003.h. or 9E003i., for any of the following aero gas turbine engines:
a. |
Specified in 9A001; or |
b. |
Whose design or production origins are either non- EU Member States or Wassenaar Arrangement Participating States; or unknown to the manufacturer. |
9A004
Space launch vehicles, "spacecraft", "spacecraft buses", "spacecraft payloads", "spacecraft" on-board systems or equipment, and terrestrial equipment, as follows
N.B.: |
SEE ALSO 9A104. |
a. |
Space launch vehicles; |
b. |
"Spacecraft"; |
c. |
"Spacecraft buses"; |
d. |
"Spacecraft payloads" incorporating items specified in 3A001.b.1.a.4., 3A002.g., 5A001.a.1., 5A001.b.3., 5A002.c., 5A002.e., 6A002.a.1., 6A002.a.2., 6A002.b., 6A002.d., 6A003.b., 6A004.c., 6A004.e., 6A008.d., 6A008.e., 6A008.k., 6A008.l. or 9A010.c.; |
e. |
On-board systems or equipment, specially designed for "spacecraft" and having any of the following functions:
|
f. |
Terrestrial equipment, specially designed for "spacecraft" as follows:
|
9A005
Liquid rocket propulsion systems containing any of the systems or components, specified in 9A006.
N.B.: |
SEE ALSO 9A105 AND 9A119. |
9A006
Systems and components, specially designed for liquid rocket propulsion systems, as follows:
N.B.: |
SEE ALSO 9A106, 9A108 AND 9A120. |
a. |
Cryogenic refrigerators, flightweight dewars, cryogenic heat pipes or cryogenic systems, specially designed for use in space vehicles and capable of restricting cryogenic fluid losses to less than 30 % per year; |
b. |
Cryogenic containers or closed-cycle refrigeration systems, capable of providing temperatures of 100 K (– 173 °C) or less for "aircraft" capable of sustained flight at speeds exceeding Mach 3, launch vehicles or "spacecraft"; |
c. |
Slush hydrogen storage or transfer systems; |
d. |
High pressure (exceeding 17,5 MPa) turbo pumps, pump components or their associated gas generator or expander cycle turbine drive systems; |
e. |
High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor; |
f. |
Propellant storage systems using the principle of capillary containment or positive expulsion (i.e., with flexible bladders); |
g. |
Liquid propellant injectors with individual orifices of 0,381 mm or smaller in diameter (an area of 1,14 × 10– 3 cm2 or smaller for non-circular orifices) and specially designed for liquid rocket engines; |
h. |
One-piece carbon-carbon thrust chambers or one-piece carbon-carbon exit cones, with densities exceeding 1,4 g/cm3 and tensile strengths exceeding 48 MPa. |
9A007
Solid rocket propulsion systems having any of the following:
N.B.: |
SEE ALSO 9A107 AND 9A119. |
a. |
Total impulse capacity exceeding 1,1 MNs; |
b. |
Specific impulse of 2,4 kNs/kg or more, when the nozzle flow is expanded to ambient sea level conditions for an adjusted chamber pressure of 7 MPa; |
c. |
Stage mass fractions exceeding 88 % and propellant solid loadings exceeding 86 %; |
d. |
Components specified in 9A008; or |
e. |
Insulation and propellant bonding systems, using direct-bonded motor designs to provide a 'strong mechanical bond' or a barrier to chemical migration between the solid propellant and case insulation material. Technical Note: 'Strong mechanical bond' means bond strength equal to or more than propellant strength. |
9A008
Components specially designed for solid rocket propulsion systems, as follows:
N.B.: |
SEE ALSO 9A108. |
a. |
Insulation and propellant bonding systems, using liners to provide a 'strong mechanical bond' or a barrier to chemical migration between the solid propellant and case insulation material; Technical Note: 'Strong mechanical bond' means bond strength equal to or more than propellant strength. |
b. |
Filament-wound "composite" motor cases exceeding 0,61 m in diameter or having 'structural efficiency ratios (PV/W)' exceeding 25 km; Technical Note: 'Structural efficiency ratio (PV/W)' is the burst pressure (P) multiplied by the vessel volume (V) divided by the total pressure vessel weight (W). |
c. |
Nozzles with thrust levels exceeding 45 kN or nozzle throat erosion rates of less than 0,075 mm/s; |
d. |
Movable nozzle or secondary fluid injection thrust vector control systems, capable of any of the following:
|
9A009
Hybrid rocket propulsion systems having any of the following:
N.B.: |
SEE ALSO 9A109 AND 9A119. |
a. |
Total impulse capacity exceeding 1,1 MNs; or |
b. |
Thrust levels exceeding 220 kN in vacuum exit conditions. |
9A010
Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or "spacecraft", as follows:
N.B.: |
SEE ALSO 1A002 AND 9A110. |
a. |
Components and structures, each exceeding 10 kg and specially designed for launch vehicles manufactured using any of the following:
|
b. |
Components and structures, specially designed for launch vehicle propulsion systems specified in 9A005 to 9A009 manufactured using any of the following:
|
c. |
Structural components and isolation systems, specially designed to control actively the dynamic response or distortion of "spacecraft" structures; |
d. |
Pulsed liquid rocket engines with thrust-to-weight ratios equal to or more than 1 kN/kg and a response time (the time required to achieve 90 % of total rated thrust from start-up) of less than 30 ms. |
9A011
Ramjet, scramjet or combined cycle engines, and specially designed components therefor.
N.B.: |
SEE ALSO 9A111 AND 9A118. |
9A012
"Unmanned aerial vehicles" ("UAVs"), unmanned "airships", related, equipment and components, as follows:
N.B.: |
SEE ALSO 9A112. |
a. |
"UAVs" or unmanned "airships", designed to have controlled flight out of the direct 'natural vision' of the 'operator' and having any of the following:
|
b. |
Related equipment and components, as follows:
|
9A101
Turbojet and turbofan engines, other than those specified in 9A001, as follows;
a. |
Engines having both of the following characteristics:
Technical Note: For the purpose of 9A101.a.1. 'maximum thrust value' is the manufacturer's demonstrated maximum thrust for the engine type un-installed. The civil type certified thrust value will be equal or less than the manufacturer's demonstrated maximum thrust for the engine type. |
b. |
Engines designed or modified for use in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a, |
9A102
'Turboprop engine systems' specially designed for unmanned aerial vehicles specified in 9A012 or 9A112.a, and specially designed components therefor, having a 'maximum power' greater than 10 kW.
Note: |
9A102 does not control civil certified engines. |
Technical Notes:
1. |
For the purposes of 9A102 a 'turboprop engine system' incorporates all of the following:
|
2. |
For the purposes of 9A102 the 'maximum power' is achieved uninstalled at sea level static conditions using ICAO standard atmosphere. |
9A104
Sounding rockets, capable of a range of at least 300 km.
N.B.: |
SEE ALSO 9A004. |
9A105
Liquid propellant rocket engines or gel propellant rocket motors, as follows:
N.B.: |
SEE ALSO 9A119. |
a. |
Liquid propellant rocket engines or gel propellant rocket motors, usable in "missiles", other than those specified in 9A005, integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 MNs; |
b. |
Liquid propellant rocket engines or gel propellant rocket motors, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005 or 9A105.a., integrated, or designed or modified to be integrated, into a liquid propellant or gel propellant propulsion system which has a total impulse capacity equal to or greater than 0,841 MNs. |
9A106
Systems or components, other than those specified in 9A006 as follows, specially designed for liquid rocket propulsion systems:
a. |
Not used; |
b. |
Rocket nozzles and combustion chambers, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; |
c. |
Thrust vector control sub-systems, usable in "missiles"; Technical Note: Examples of methods of achieving thrust vector control specified in 9A106.c. are:
|
d. |
Liquid, slurry and gel propellant (including oxidisers) control systems, and specially designed components therefor, usable in "missiles", designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.
|
e. |
Combustion chambers and nozzles, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
9A107
Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.
N.B.: |
SEE ALSO 9A119. |
9A108
Components, other than those specified in 9A008, as follows, specially designed for solid rocket propulsion systems:
a. |
Rocket motor cases and "insulation" components therefor, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; |
b. |
Rocket nozzles, usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; |
c. |
Thrust vector control sub-systems, usable in "missiles". Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are:
|
9A109
Hybrid rocket motors and specially designed components as follows:
a. |
Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor; |
b. |
Specially designed components for hybrid rocket motors specified in 9A009 that are usable in "missiles". |
N.B.: |
SEE ALSO 9A009 and 9A119. |
9A110
Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in 'missiles' or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
N.B.: |
SEE ALSO 1A002. |
Technical Note:
In 9A110 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
9A111
Pulse jet engines, usable in "missiles" or unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor.
N.B.: |
SEE ALSO 9A011 AND 9A118. |
9A112
"Unmanned aerial vehicles" ("UAVs"), other than those specified in 9A012, as follows:
a. |
"Unmanned aerial vehicles" ("UAVs") capable of a range of 300 km; |
b. |
"Unmanned aerial vehicles" ("UAVs") having all of the following:
Technical Notes:
|
9A115
Launch support equipment as follows:
a. |
Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, sounding rockets specified in 9A104 or unmanned aerial vehicles specified in 9A012 or 9A112.a.; |
b. |
Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. |
9A116
Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows:
a. |
Reentry vehicles; |
b. |
Heat shields and components therefor, fabricated of ceramic or ablative materials; |
c. |
Heat sinks and components therefor, fabricated of light-weight, high heat capacity materials; |
d. |
Electronic equipment specially designed for reentry vehicles. |
9A117
Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".
N.B.: |
SEE ALSO 9A121. |
9A118
Devices to regulate combustion usable in engines, which are usable in "missiles" or unmanned aerial vehicles specified in 9A012, or 9A112.a., specified in 9A011 or 9A111.
9A119
Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
9A120
Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or 'other liquid propellants', used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km.
Note: |
In 9A120 'other liquid propellants' includes, but is not limited to, propellants specified in the Military Goods Controls. |
9A121
Umbilical and interstage electrical connectors specially designed for "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Technical Note:
Interstage connectors referred to in 9A121 also include electrical connectors installed between the "missile", space launch vehicle or sounding rocket and their payload.
9A350
Spraying or fogging systems, specially designed or modified for fitting to aircraft, "lighter-than-air vehicles" or unmanned aerial vehicles, and specially designed components therefor, as follows:
a. |
Complete spraying or fogging systems capable of delivering, from a liquid suspension, an initial droplet 'VMD' of less than 50 μm at a flow rate of greater than two litres per minute; |
b. |
Spray booms or arrays of aerosol generating units capable of delivering, from a liquid suspension, an initial droplet 'VMD' of less than 50 μm at a flow rate of greater than two litres per minute; |
c. |
Aerosol generating units specially designed for fitting to systems specified in 9A350.a. and b.
|
Note: |
9A350 does not control spraying or fogging systems and components that are demonstrated not to be capable of delivering biological agents in the form of infectious aerosols. |
Technical Notes:
1. |
Droplet size for spray equipment or nozzles specially designed for use on aircraft, "lighter-than-air vehicles" or unmanned aerial vehicles should be measured using either of the following:
|
2. |
In 9A350 'VMD' means Volume Median Diameter and for water-based systems this equates to Mass Median Diameter (MMD). |
9B
Test, Inspection and Production Equipment
9B001
Equipment, tooling or fixtures, specially designed for manufacturing gas turbine blades, vanes or "tip shroud" castings, as follows:
a. |
Directional solidification or single crystal casting equipment; |
b. |
Casting tooling, manufactured from refractory metals or ceramics, as follows:
|
c. |
Directional-solidification or single-crystal additive-manufacturing equipment. |
9B002
On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, having all of the following:
a. |
Specially designed for the "development" of gas turbine engines, assemblies or components; and |
b. |
Incorporating "technology" specified in 9E003.h. or 9E003.i. |
9B003
Equipment specially designed for the "production" or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.
9B004
Tools, dies or fixtures, for the solid state joining of "superalloy", titanium or intermetallic airfoil-to-disk combinations described in 9E003.a.3. or 9E003.a.6. for gas turbines.
9B005
On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following:
N.B.: |
SEE ALSO 9B105. |
a. |
Wind tunnels designed for speeds of Mach 1,2 or more;
|
b. |
Devices for simulating flow-environments at speeds exceeding Mach 5, including hot-shot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns; or |
c. |
Wind tunnels or devices, other than two-dimensional sections, capable of simulating Reynolds number flows exceeding 25 × 106. |
9B006
Acoustic vibration test equipment capable of producing sound pressure levels of 160 dB or more (referenced to 20 μPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1 273 K (1 000 °C), and specially designed quartz heaters therefor.
N.B.: |
SEE ALSO 9B106. |
9B007
Equipment specially designed for inspecting the integrity of rocket motors and using Non-Destructive Test (NDT) techniques other than planar x-ray or basic physical or chemical analysis.
9B008
Direct measurement wall skin friction transducers specially designed to operate at a test flow total (stagnation) temperature exceeding 833 K (560 °C).
9B009
Tooling specially designed for producing turbine engine powder metallurgy rotor components capable of operating at stress levels of 60 % of Ultimate Tensile Strength (UTS) or more and metal temperatures of 873 K (600 °C) or more.
9B010
Equipment specially designed for the production of items specified in 9A012.
9B105
'Aerodynamic test facilities' for speeds of Mach 0,9 or more, usable for 'missiles' and their subsystems.
N.B.: |
SEE ALSO 9B005. |
Note: |
9B105 does not control wind-tunnels for speeds of Mach 3 or less with dimension of the 'test cross section size' equal to or less than 250 mm. |
Technical Notes:
1. |
In 9B105 'aerodynamic test facilities' includes wind tunnels and shock tunnels for the study of airflow over objects. |
2. |
In Note to 9B105, 'test cross section size' means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest 'test cross section' location. 'Test cross section' is the section perpendicular to the flow direction. |
3. |
In 9B105 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
9B106
Environmental chambers and anechoic chambers, as follows:
a. |
Environmental chambers having all the following:
Technical Notes:
|
b. |
Environmental chambers capable of simulating the following flight conditions:
|
9B115
Specially designed "production equipment" for the systems, sub-systems and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A105 to 9A109, 9A111, 9A116 to 9A120.
9B116
Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, 9A011, 9A101, 9A102, 9A104 to 9A109, 9A111, 9A116 to 9A120 or 'missiles'.
Technical Note:
In 9B116 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
9B117
Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics:
a. |
The capacity to handle more than 68 kN of thrust; or |
b. |
Capable of simultaneously measuring the three axial thrust components. |
9C
Materials
9C108
"Insulation" material in bulk form and "interior lining", other than those specified in 9A008, for rocket motor cases usable in "missiles" or specially designed for solid propellant rocket engines specified in 9A007 or 9A107.
Technical Note:
In 9C108 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
9C110
Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a "specific tensile strength" greater than 7,62 × 104 m and a "specific modulus" greater than 3,18 × 106 m.
N.B.: |
SEE ALSO 1C010 AND 1C210. |
Note: |
The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (Tg ), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent. |
9D
Software
9D001
"Software" specially designed or modified for the "development" of equipment or "technology", specified in 9A001 to 9A119, 9B or 9E003.
9D002
"Software" specially designed or modified for the "production" of equipment specified in 9A001 to 9A119 or 9B.
9D003
"Software" incorporating "technology" specified in 9E003.h. and used in "FADEC Systems" for systems specified in 9A or equipment specified in 9B.
9D004
Other "software" as follows:
a. |
2D or 3D viscous "software", validated with wind tunnel or flight test data required for detailed engine flow modelling; |
b. |
"Software" for testing aero gas turbine engines, assemblies or components, specially designed to collect, reduce and analyse data in real time and capable of feedback control, including the dynamic adjustment of test articles or test conditions, as the test is in progress; |
c. |
"Software" specially designed to control directional solidification or single crystal material growth in equipment specified in 9B001.a. or 9B001.c.; |
d. |
Not used; |
e. |
"Software" specially designed or modified for the operation of items specified in 9A012; |
f. |
"Software" specially designed to design the internal cooling passages of aero gas turbine blades, vans and "tip shrouds"; |
g. |
"Software" having all of the following:
|
9D005
"Software" specially designed or modified for the operation of items specified in 9A004.e. or 9A004.f.
9D101
"Software" specially designed or modified for the "use" of goods specified in 9B105, 9B106, 9B116 or 9B117.
9D103
"Software" specially designed for modelling, simulation or design integration of the space launch vehicles specified in 9A004 sounding rockets specified in 9A104 or "missiles", or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
Note: |
"Software" specified in 9D103 remains controlled when combined with specially designed hardware specified in 4A102. |
9D104
"Software" as follows:
a. |
"Software" specially designed or modified for the "use" of goods specified in 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A009.a., 9A010.d., 9A011, 9A101, 9A102, 9A105, 9A106.d., 9A107, 9A109, 9A111, 9A115.a., 9A117 or 9A118. |
b. |
"Software" specially designed or modified for the operation or maintenance of subsystems or equipment specified in 9A008.d., 9A106.c., 9A108.c. or 9A116.d. |
9D105
"Software" specially designed or modified to coordinate the function of more than one subsystem, other than that specified in 9D004.e., in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.or 'missiles'
Technical Note:
In 9D105 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
9E
Technology
Note: |
"Development" or "production" "technology" specified in 9E001 to 9E003 for gas turbine engines remains controlled when used for repair or overhaul. Excluded from control are: technical data, drawings or documentation for maintenance activities directly associated with calibration, removal or replacement of damaged or unserviceable line replaceable units, including replacement of whole engines or engine modules. |
9E001
"Technology" according to the General Technology Note for the "development" of equipment or "software", specified in 9A001.b., 9A004 to 9A012, 9A350, 9B or 9D.
9E002
"Technology" according to the General Technology Note for the "production" of equipment specified in 9A001.b., 9A004 to 9A011, 9A350 or 9B.
N.B.: |
For "technology" for the repair of controlled structures, laminates or materials, see 1E002.f. |
9E003
Other "technology" as follows:
a. |
"Technology" "required" for the "development" or "production" of any of the following gas turbine engine components or systems:
|
b. |
"Technology" "required" for the "development" or "production" of any of the following:
|
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:
Technical Notes:
|
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:
Technical Note: 'Box volume' in 9E003.e. is the product of three perpendicular dimensions measured in the following way:
|
f. |
"Technology" "required" for the "production" of specially designed components for high output diesel engines, as follows:
|
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:
|
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:
|
j. |
"Technology" "required" for the "development" of wing-folding systems designed for fixed-wing "aircraft" powered by gas turbine engines.
|
9E101
a. |
"Technology" according to the General Technology Note for the "development" of goods specified in 9A101, 9A102, 9A104 to 9A111, 9A112.a. or 9A115 to 9A121. |
b. |
"Technology" according to the General Technology Note for the "production" of 'UAV's specified in 9A012 or goods specified in. 9A101, 9A102, 9A104 to 9A111, 9A112.a. 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 in 9A004, goods specified in 9A005 to 9A011, 'UAV's specified in 9A012 or goods specified in 9A101, 9A102, 9A104 to 9A111, 9A112.a., 9A115 to 9A121, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9D103.
Technical Note:
In 9E102 'UAV' means unmanned aerial vehicle systems capable of a range exceeding 300 km.’
(1) Manufacturers calculating positioning accuracy in accordance with ISO 230-2:1977 or 2006 should consult the competent authorities of the Member State in which they are established.
(2) Manufacturers calculating positioning accuracy in accordance with ISO 230-2:1977 or 2006 should consult the competent authorities of the Member State in which they are established.
(*1) The numbers in parenthesis refer to the Notes following this Table.
ANNEX II
‘ANNEX IIa
UNION GENERAL EXPORT AUTHORISATION NO EU001
(referred to in Article 9(1) of this Regulation)
Exports to Australia, Canada, Japan, New Zealand, Norway, Switzerland, including Liechtenstein, and United States of America
Issuing authority: European Commission
Part 1
This general export authorisation covers all dual-use items specified in any entry in Annex I to this Regulation, except those listed in Annex IIg.
Part 2
This export authorisation is valid throughout the Union for exports to the following destinations:
— |
Australia |
— |
Canada |
— |
Japan |
— |
New Zealand |
— |
Norway |
— |
Switzerland, including Lichtenstein |
— |
United States of America |
Conditions and requirements for use of this authorisation
1. |
Exporters that use this authorisation shall notify the competent authorities of the Member State where they are established of their first use of this authorisation no later than 30 days after the date when the first export took place.
Exporters shall also report in the Single Administrative Document the fact that they are using this authorisation EU 001 by indicating in box 44 the reference X002. |
2. |
This authorisation may not be used if:
|
3. |
Reporting requirements attached to the use of this authorisation and the additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States.
A Member State may require the exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within ten working days of receipt. Where applicable the requirements set out in the first two paragraphs of this point shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations. |
‘ANNEX IIb
UNION GENERAL EXPORT AUTHORISATION NO EU002
(referred to in Article 9(1) of this Regulation)
Exports of certain dual-use items to certain destinations
Issuing authority: European Union
Part 1 — Items
This general export authorisation covers the following dual-use items specified in Annex I to this Regulation:
— |
1A001, |
— |
1A003, |
— |
1A004, |
— |
1C003b-c, |
— |
1C004, |
— |
1C005, |
— |
1C006, |
— |
1C008, |
— |
1C009, |
— |
2B008, |
— |
3A001a3, |
— |
3A001a6-12, |
— |
3A002c-f, |
— |
3C001, |
— |
3C002, |
— |
3C003, |
— |
3C004, |
— |
3C005, |
— |
3C006. |
Part 2 — Destinations
This authorisation is valid throughout the Union for exports to the following destinations:
— |
Argentina, |
— |
Croatia, |
— |
Iceland, |
— |
South Africa, |
— |
South Korea, |
— |
Turkey. |
Part 3 — Conditions and requirements for use
1. |
This authorisation does not authorise the export of items where:
|
2. |
Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU002 in box 44 of the Single Administrative Document. |
3. |
Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.
Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States. A Member State may require the exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation. Where applicable the requirements set out in the second and third paragraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations. |
‘ANNEX IIc
UNION GENERAL EXPORT AUTHORISATION NO EU003
(referred to in Article 9(1) of this Regulation)
Export after repair/replacement
Issuing authority: European Union
Part 1 — Items
1. |
This general export authorisation covers all dual-use items specified in any entry in Annex I to this Regulation except those listed in paragraph 2 where:
|
2. |
Items excluded:
|
Part 2 — Destinations
This authorisation is valid throughout the Union for exports to the following destinations:
Albania |
Argentina |
Bosnia and Herzegovina |
Brazil |
Chile |
China (including Hong Kong and Macao) |
Croatia |
former Yugoslav Republic of Macedonia, the |
French Overseas Territories |
Iceland |
India |
Kazakhstan |
Mexico |
Montenegro |
Morocco |
Russia |
Serbia |
Singapore |
South Africa |
South Korea |
Tunisia |
Turkey |
Ukraine |
United Arab Emirates |
Part 3 — Conditions and requirements for use
1. |
This authorisation can only be used when the initial export has taken place under a Union General Export Authorisation or an initial export authorisation has been granted by the competent authorities of the Member State where the original exporter was established for the export of the items which have subsequently been reimported into the customs territory of the European Union for the purposes of maintenance, repair or replacement. This authorisation is valid only for exports to the original end-user. |
2. |
This authorisation does not authorise the export of items where:
|
3. |
On exportation of any of the items pursuant to this authorisation, exporters must:
|
4. |
Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.
Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States. A Member State may require the exporter established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation. Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations. |
5. |
This authorisation covers items for 'repair', 'replacement' and 'maintenance'. This may involve coincidental improvement on the original goods, e.g. resulting from the use of modern spare parts or from use of a later built standard for reliability or safety reasons, provided that this does not result in any enhancement to the functional capability of the items or provide the items with new or additional functions. |
‘ANNEX IId
UNION GENERAL EXPORT AUTHORISATION NO EU004
(referred to in Article 9(1) of this Regulation)
Temporary export for exhibition or fair
Issuing authority: European Union
Part 1 — Items
This general export authorisation covers all dual-use items specified in any entry in Annex I to this Regulation except:
(a) |
all items listed in Annex IIg; |
(b) |
all items in Section D set out in Annex I to this Regulation (this does not include software necessary to the proper functioning of the equipment for the purpose of the demonstration); |
(c) |
all items in Section E set out in Annex I to this Regulation; |
(d) |
the following items specified in Annex I to this Regulation:
|
Part 2 — Destinations
This authorisation is valid throughout the Union for exports to the following destinations:
Albania, Argentina, Bosnia and Herzegovina, Brazil, Chile, China (including Hong Kong and Macao), Croatia, the former Yugoslav Republic of Macedonia, French Overseas Territories, Iceland, India, Kazakhstan, Mexico, Montenegro, Morocco, Russia, Serbia, Singapore, South Africa, South Korea, Tunisia, Turkey, Ukraine, and United Arab Emirates.
Part 3 — Conditions and requirements for use
1. |
This authorisation authorises the export of items listed in Part 1 on condition that the export concerns temporary export for exhibition or fair as defined in point 6 and that the items are reimported within a period of 120 days after the initial export, complete and without modification, into the customs territory of the European Union. |
2. |
The competent authority of the Member State where the exporter is established as defined in Article 9(6) of this Regulation may, at the exporter's request, waive the requirement that the items are to be reimported as stated in paragraph 1. To waive the requirement, the procedure for individual authorisations laid down in Articles 9(2) and 14(1) of this Regulation shall apply accordingly. |
3. |
This authorisation does not authorise the export of items where:
|
4. |
Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU004 in box 44 of the Single Administrative Document. |
5. |
Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.
Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States. A Member State may require exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation. Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations. |
6. |
For the purpose of this authorisation, 'exhibition or fair' means commercial events of a specific duration at which several exhibitors make demonstrations of their products to trade visitors or to the general public. |
‘ANNEX IIe
UNION GENERAL EXPORT AUTHORISATION NO EU005
(referred to in Article 9(1) of this Regulation)
Telecommunications
Issuing authority: European Union
Part 1 — Items
This general export authorisation covers the following dual-use items specified in Annex I to this Regulation:
(a) |
the following items of Category 5, Part l:
|
(b) |
technology controlled by 5E001a, where required for the installation, operation, maintenance or repair of items specified under (a) and intended for the same end-user. |
Part 2 — Destinations
This authorisation is valid throughout the Union for exports to the following destinations:
Argentina, China (including Hong Kong and Macao), Croatia, India, Russia, South Africa, South Korea, Turkey, and Ukraine.
Part 3 — Conditions and requirements for use
1. |
This authorisation does not authorise the export of items where:
|
2. |
Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU005 in box 44 of the Single Administrative Document. |
3. |
Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.
Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States. A Member State may require exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation. Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations. |
‘ANNEX IIf
UNION GENERAL EXPORT AUTHORISATION NO EU006
(referred to in Article 9(1) of this Regulation)
Chemicals
Part 1 — Items
This general export authorisation covers the following dual-use items specified in Annex I to this Regulation:
1C350: |
|
1C450 a: |
|
1C450 b: |
|
Part 2 — Destinations
This authorisation is valid throughout the Union for exports to the following destinations:
Argentina, Croatia, Iceland, South Korea, Turkey, and Ukraine.
Part 3 — Conditions and requirements for use
1. |
This authorisation does not authorise the export of items where:
|
2. |
Exporters must mention the EU reference number X002 and specify that the items are being exported under Union General Export Authorisation EU006 in box 44 of the Single Administrative Document. |
3. |
Any exporter who uses this authorisation must notify the competent authorities of the Member State where he is established of the first use of this authorisation no later than 30 days after the date when the first export took place or, alternatively, and in accordance with a requirement by the competent authority of the Member State where the exporter is established, prior to the first use of this authorisation. Member States shall notify the Commission of the notification mechanism chosen for this authorisation. The Commission shall publish the information notified to it in the C series of the Official Journal of the European Union.
Reporting requirements attached to the use of this authorisation and additional information that the Member State from which the export is made might require on items exported under this authorisation are defined by Member States. A Member State may require exporters established in that Member State to register prior to the first use of this authorisation. Registration shall be automatic and acknowledged by the competent authorities to the exporter without delay and in any case within 10 working days of receipt, subject to Article 9(1) of this Regulation. Where applicable the requirements set out in the second and third subparagraphs shall be based on those defined for the use of national general export authorisations granted by those Member States which provide for such authorisations. |
‘ANNEX IIg
(List referred to in Article 9(4)(a) of this Regulation and Annexes IIa, IIc and IId to this Regulation)
The entries do not always provide a complete description of the items and the related notes in Annex I. Only Annex I provides a complete description of the items.
The mention of an item in this Annex does not affect the application of the General Software Note (GSN) in Annex I.
— |
all items specified in Annex IV, |
— |
0C001 "Natural uranium" or "depleted uranium" or thorium in the form of metal, alloy, chemical compound or concentrate and any other material containing one or more of the foregoing, |
— |
0C002 "Special fissile materials" other than those specified in Annex IV, |
— |
0D001 "Software" specially designed or modified for the "development", "production" or "…" of goods specified in Category 0, in so far as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV, |
— |
0E001 "Technology" in accordance with the Nuclear Technology Note for the "development", "production" or "…" of goods specified in Category 0, in so far as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV, |
— |
1A102 Resaturated pyrolised carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104, |
— |
1C351 Human and animal pathogens and "toxins", |
— |
1C353 Genetic elements and genetically modified organisms, |
— |
1C354 Plant pathogens, |
— |
1C450a.1. amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (78-53-5) and corresponding alkylated or protonated salts, |
— |
1C450a.2. PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (382-21-8), |
— |
7E104 "Technology" for the integration of flight control, guidance and propulsion data into a flight management system for optimisation of rocket system trajectory, |
— |
9A009.a. Hybrid rocket propulsion systems with total impulse capacity exceeding 1,1 MNs, |
— |
9A117 Staging mechanisms, separation mechanisms and interstages usable in "missiles". |
ANNEX III
‘ANNEX IV
(List referred to in Article 22(1) of this Regulation)
The entries do not always cover the complete description of the item and the related notes in Annex I (1). Only Annex I provides for the complete description of the items.
The mention of an item in this Annex does not affect the application of the provisions concerning mass-market products in Annex I.
PART I
(possibility of National General Authorisation for intra-Community trade)
Items of stealth technology
1C001 |
Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers.
|
||
1C101 |
Materials or devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures; other than those specified in 1C001, usable in "missiles", 'missile' subsystems or unmanned aerial vehicles specified in 9A012.
Technical Note: In 1C101 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km. |
||
1D103 |
"Software" specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures. |
||
1E101 |
"Technology" according to the GTN for the "use" of goods specified in 1C101 or 1D103. |
||
1E102 |
"Technology" according to the GTN for the "development" of "software" specified in 1D103. |
||
6B008 |
Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less and specially designed components therefor.
|
||
6B108 |
Systems specially designed for radar cross section measurement usable for "missiles" and their subsystems. |
Items of the Community strategic control
1A007 |
Equipment and devices, specially designed to initiate charges and devices containing energetic materials, by electrical means, as follows:
|
||||||||||||||||
1C239 |
High explosives, other than those specified in the Military Goods Controls, 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. |
||||||||||||||||
1E201 |
"Technology" according to the General Technology Note for the "use" of goods specified in 1C239. |
||||||||||||||||
3A229 |
High-current pulse generators, as follows …
|
||||||||||||||||
3A232 |
Multipoint initiation systems, other than those specified in 1A007 above , as follows…
|
||||||||||||||||
3E201 |
"Technology" according to the General Technology Note for the "use" of equipment specified in 3A228.a., 3A228.b. or 3A231. |
||||||||||||||||
6A001 |
Acoustics, limited to the following: |
||||||||||||||||
6A001.a.1.b. |
Object detection or location systems having any of the following:
|
||||||||||||||||
6A001.a.2.a.2. |
Hydrophones … Incorporating … |
||||||||||||||||
6A001.a.2.a.3. |
Hydrophones … Having any … |
||||||||||||||||
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 systems having any of the following:
|
||||||||||||||||
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; |
||||||||||||||||
6D003.a. |
"Software" for the "real time processing" of acoustic data; |
||||||||||||||||
8A002.o.3. |
Noise reduction systems designed for use on vessels of 1 000 tonnes displacement or more, as follows:
|
||||||||||||||||
8E002.a. |
"Technology" for the "development", "production", repair, overhaul or refurbishing (re-machining) of propellers specially designed for underwater noise reduction. |
Items of the Community strategic control — Cryptography — Category 5 Part 2
5A004 |
Equipment designed or modified to perform "cryptanalytic functions".
Technical Note: "Cryptanalytic functions" are functions designed to defeat cryptographic mechanisms in order to derive confidential variables or sensitive data, including clear text, passwords or cryptographic keys. |
||
5D002.c.1 |
Only software having the characteristics, or performing or simulating the functions, of equipment specified in 5A004. |
||
5E002.a. |
Only "technology" for the "development", "production" or "use" of the goods specified in 5A004 or 5D002.c.1. above. |
Items of the MTCR technology
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 . |
||||||||||||
7B001 |
Test, calibration or alignment equipment specially designed for equipment specified in 7A117 above.
|
||||||||||||
7B003 |
Equipment specially designed for the "production" of equipment specified in 7A117 above. |
||||||||||||
7B103 |
"Production facilities" specially designed for equipment specified in 7A117 above . |
||||||||||||
7D101 |
"Software" specially designed for the "use" of equipment specified in 7B003 or 7B103 above . |
||||||||||||
7E001 |
"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 7A117, 7B003, 7B103 or 7D101 above . |
||||||||||||
7E002 |
"Technology" according to the General Technology Note for the "production" of equipment specified in 7A117, 7B003 and 7B103 above . |
||||||||||||
7E101 |
"Technology" according to the General Technology Note for the "use" of equipment specified in 7A117, 7B003, 7B103 and 7D101 above . |
||||||||||||
9A004 |
Space launch vehicles capable of delivering at least a 500 kg payload to a range of at least 300 km .
|
||||||||||||
9A005 |
Liquid rocket propulsion systems containing any of the systems or components specified in 9A006 usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below .
|
||||||||||||
9A007.a. |
Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below , with any of the following:
|
||||||||||||
9A008.d. |
Components, as follows, specially designed for solid rocket propulsion systems:
|
||||||||||||
9A104 |
Sounding rockets, capable of delivering at least a 500 kg payload to a range of at least 300 km.
|
||||||||||||
9A105.a. |
Liquid propellant rocket engines, as follows:
|
||||||||||||
9A106.c. |
Systems or components, other than those specified in 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems:
Technical Note: Examples of methods of achieving thrust vector control specified in 9A106.c. are:
|
||||||||||||
9A108.c. |
Components, other than those specified in 9A008, usable in "missiles" as follows, specially designed for solid rocket propulsion systems:
Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are:
|
||||||||||||
9A116 |
Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows, except for reentry vehicles designed for non-weapon payloads :
|
||||||||||||
9A119 |
Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of delivering at least a 500 kg payload to a range of 300 km, other than those specified in 9A005 or 9A007.a. above |
||||||||||||
9B115 |
Specially designed "production equipment" for the systems, sub-systems and components specified in 9A005, 9A007.a., 9A008.d., 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above . |
||||||||||||
9B116 |
Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above . |
||||||||||||
9D101 |
"Software" specially designed for the "use" of goods specified in 9B116 above . |
||||||||||||
9E001 |
"Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115, 9B116 or 9D101 above . |
||||||||||||
9E002 |
"Technology" according to the General Technology Note for the "production" of equipment specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115 or 9B116 above .
|
||||||||||||
9E101 |
"Technology" according to the General Technology Note for the "development" or "production" of goods specified in 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above . |
||||||||||||
9E102 |
"Technology" according to the General Technology Note for the "use" of space launch vehicles specified in 9A004, 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116, 9A119, 9B115, 9B116 or 9D101 above . |
Exemptions:
Annex IV does not control the following items of the MTCR technology:
1. |
that are transferred on the basis of orders pursuant to a contractual relationship placed by the European Space Agency (ESA) or that are transferred by ESA to accomplish its official tasks; |
2. |
that are transferred on the basis of orders pursuant to a contractual relationship placed by a Member State's national space organisation or that are transferred by it to accomplish its official tasks; |
3. |
that are transferred on the basis of orders pursuant to a contractual relationship placed in connection with a Community space launch development and production programme signed by two or more European governments; |
4. |
that are transferred to a State-controlled space launching site in the territory of a Member State, unless that Member State controls such transfers within the terms of this Regulation. |
PART II
(no National General Authorisation for intra-Community trade)
Items of the CWC (Chemical Weapons Convention)
1C351.d.4. |
Ricin |
1C351.d.5. |
Saxitoxin |
Items of the NSG technology
All Category 0 of Annex I is included in Annex IV, subject to the following:
— |
0C001: this item is not included in Annex IV. |
— |
0C002: this item is not included in Annex IV, with the exception of special fissile materials as follows:
|
— |
0C003 only if for use in a "nuclear reactor" (within 0A001.a) |
— |
0D001 (software) is included in Annex IV except insofar as it relates to 0C001 or to those items of 0C002 that are excluded from Annex IV. |
— |
0E001 (technology) is included in Annex IV except insofar as these related to 0C001 or to those items of 0C002 that are excluded from Annex IV. |
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.
|
||||||||||||||||||
1C012 |
Materials as follows: Technical Note: These materials are typically used for nuclear heat sources.
|
||||||||||||||||||
1B231 |
Tritium facilities or plants, and equipment therefor, as follows:
|
||||||||||||||||||
1B233 |
Lithium isotope separation facilities or plants, and equipment therefor, 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.
Technical Note: The natural isotopic abundance of lithium-6 is approximately 6,5 weight % (7,5 atom %). |
||||||||||||||||||
1C235 |
Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1 000 , and products or devices containing any of the foregoing.
|
||||||||||||||||||
1E001 |
"Technology" according to the General Technology Note for the "development" or "production" of equipment or materials specified in 1C012.b. |
||||||||||||||||||
1E201 |
"Technology" according to the General Technology Note for the "use" of goods specified in 1B226, 1B231, 1B233, 1C233 or 1C235. |
||||||||||||||||||
3A228 |
Switching devices, as follows:
|
||||||||||||||||||
3A231 |
Neutron generator systems, including tubes, having both of the following characteristics:
|
||||||||||||||||||
3E201 |
"Technology" according to the General Technology Note for the "use" of equipment specified in 3A228.a., 3A228.b. or 3A231. |
||||||||||||||||||
6A203 |
Cameras and components, other than those specified in 6A003, as follows:
|
||||||||||||||||||
6A225 |
Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.
|
||||||||||||||||||
6A226 |
Pressure sensors, as follows:
|
(1) The differences in the wordings/scopes between Annex I and Annex IV are indicated with bold italic text.