Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers.

N.B. SEE ALSO 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.

Note: 1C101 does not control materials if such goods are formulated solely for civil applications.

Technical Note: In 1C101 ‘missiles’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

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

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 multiple controlled detonators specified in 1A007.b. below ;

b. Electrically driven explosive detonators as follows:

1. Exploding bridge (EB);

2. Exploding bridge wire (EBW);

3. Slapper;

4. Exploding foil initiators (EFI).

Note: 1A007.b. does not control detonators using only primary explosives, such as lead azide.

High-current pulse generators, as follows:

N.B. SEE ALSO MILITARY GOODS CONTROLS

Multipoint initiation systems, other than those specified in 1A007 above , as follows:

N.B. SEE ALSO MILITARY GOODS CONTROLS

Object detection or location systems having any of the following:

1. A transmitting frequency below 5 kHz; 6. Designed to withstand;

Bottom or bay cable systems having any of the following:

1. Incorporating hydrophones or

2. Incorporating multiplexed hydrophone group signal modules …;

Noise reduction systems designed for use on vessels of 1 000 tonnes displacement or more, as follows:

b. Active noise reduction or cancellation systems, or magnetic bearings, specially designed for power transmission systems, and incorporating electronic control systems capable of actively reducing equipment vibration by the generation of anti-noise or anti-vibration signals directly to the source.

Equipment designed or modified to perform 'cryptanalytic functions'. Note:5A004 includes systems or equipment, designed or modified to perform 'cryptanalytic functions' by means of reverse engineering.

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.

"Software" having the characteristics of, or performing or simulating the functions of, any of the following:

3. Equipment specified in 5A004.

Test, calibration or alignment equipment specially designed for equipment specified in 7A117 above.

Note: 7B001 does not control test, calibration or alignment equipment for Maintenance Level I or Maintenance Level II.

Space launch vehicles capable of delivering at least a 500 kg payload to a range of at least 300 km .

N.B. SEE ALSO 9A104.

Note 1: 9A004 does not control payloads.

Liquid rocket propulsion systems containing any of the systems or components specified in 9A006 usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below.

N.B. SEE ALSO 9A105 and 9A119.

Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below , with any of the following:

N.B. SEE ALSO 9A119.

a. Total impulse capacity exceeding 1,1 MNs.

Components, as follows, specially designed for solid rocket propulsion systems:

N.B.SEE ALSO 9A108.c.

d. Movable nozzle or secondary fluid injection thrust vector control systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below , capable of any of the following:

1. Omni-axial movement exceeding ± 5o.

2. Angular vector rotations of 20o/s or more; or 3. Angular vector accelerations of 40o/s² or more.

Sounding rockets, capable of delivering at least a 500 kg payload to a range of at least 300 km.

N.B. SEE ALSO 9A004.

Liquid propellant rocket engines, as follows:

N.B. SEE ALSO 9A119.

a. Liquid propellant rocket engines usable in ‘missiles’, other than those specified in 9A005, integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 MNs having a total impulse capacity equal to or greater than 1,1 MNs; except liquid propellant apogee engines designed or modified for satellite applications and having all of the following:

1. nozzle throat diameter of 20 mm or less; and

2. combustion chamber pressure of 15 bar or less.

Systems or components, other than those specified in 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems:

Thrust vector control sub-systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km.

Technical Note: Examples of methods of achieving thrust vector control specified in 9A106.c. are: 1. flexible nozzle; 2. fluid or secondary gas injection; 3. movable engine or nozzle; 4. deflection of exhaust gas stream (jet vanes or probes); or 5. thrust tabs.

Components, other than those specified in 9A008, usable in ‘missiles’ as follows, specially designed for solid rocket propulsion systems: c. Thrust vector control sub-systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km.

Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are:

1. flexible nozzle;

2. fluid or secondary gas injection;

3. movable engine or nozzle;

4. deflection of exhaust gas stream (jet vanes or probes); or

5. thrust tabs.

Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows, except for reentry vehicles designed for non-weapon payloads:

a. Reentry vehicles;

b. Heat shields and components therefor fabricated of ceramic or ablative materials;

c. Heat sinks and components therefor fabricated of light-weight, high heat capacity materials;

d. Electronic equipment specially designed for reentry vehicles.

Electromagnetic isotope separators designed for, or equipped with, single or multiple ion sources capable of providing a total ion beam current of 50 mA or greater.

Note: 1B226 includes separators:

a. Capable of enriching stable isotopes;

b. With the ion sources and collectors both in the magnetic field and those configurations in which they are external to the field.

Materials as follows: Technical Note: These materials are typically used for nuclear heat sources. b.‘Previously separated’ neptunium-237 in any form.

Note: 1C012.b. does not control shipments with a neptunium-237 content of 1 g or less.

Tritium facilities or plants, and equipment therefor, as follows: a. Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;

b. Equipment for tritium facilities or plants, as follows:

1. Hydrogen or helium refrigeration units capable of cooling to 23 K (– 250 °C) or less, with heat removal capacity greater than 150 W;

2. Hydrogen isotope storage or purification systems using metal hydrides as the storage or purification medium.

Lithium isotope separation facilities or plants, and equipment therefor, as follows:

a. Facilities or plants for the separation of lithium isotopes;

b. Equipment for the separation of lithium isotopes, as follows:

1. Packed liquid-liquid exchange columns specially designed for lithium amalgams;

2. Mercury or lithium amalgam pumps;

3. Lithium amalgam electrolysis cells;

4. Evaporators for concentrated lithium hydroxide solution.

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 % (7,5 atom %).

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:1 C235 does not control a product or device containing less than 1,48 × 103 GBq (40 Ci) of tritium.

Switching devices, as follows: a. Cold-cathode tubes, whether gas filled or not, operating similarly to a spark gap, having all of the following characteristics:

1. Containing three or more electrodes;

2. Anode peak voltage rating of 2,5 kV or more;

3. Anode peak current rating of 100 A or more; and

4. Anode delay time of 10 μs or less.

Note: 3A228 includes gas krytron tubes and vacuum sprytron tubes.

b. Triggered spark-gaps having both of the following characteristics

1. An anode delay time of 15 μs or less; and

2. Rated for a peak current of 500 A or more.

Neutron generator systems, including tubes, having both of the following characteristics:

a. Designed for operation without an external vacuum system; and b. utilising electrostatic acceleration to induce a tritium-deuterium nuclear reaction.

Cameras and components, other than those specified in 6A003, as follows:

a. Mechanical rotating mirror streak cameras, as follows, and specially designed components therefor:

1. Streak cameras with writing speeds greater than 0,5 mm per microsecond;

b. Mechanical rotating mirror framing cameras, as follows, and specially designed components therefor:

1. Framing cameras with recording rates greater than 225 000 frames per second;

Note: In 6A203.a. components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors and bearings.

Velocity interferometers for measuring velocities exceeding 1 km/s during time intervals of less than 10 microseconds.

Note: 6A225 includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).

Pressure sensors, as follows:

a. Manganin gauges for pressures greater than 10 GPa;

b. Quartz pressure transducers for pressures greater than 10 GPa.

• Indication of the commercial reference of the cryptology mean, and of the version.
  General description of the means and its features.
  Indication of the category in which the means is to be classified (Personal computer encryption software. Operating system. Electronic messaging. Wireless communication system. Network encryption means. Telephone or fax. Other (to be specified)

• Presentation of the cryptology services provided (Authentication. Signature Integrity checking. Confidentiality. Timestamping. Secure archiving. Cryptographic key management. Key or data certification. Other (to be specified). Specify the names of the algorithms used and the maximum length of the cryptographic keys for each algorithm.

• Presentation of the implementation of the algorithms (software, hardware).

• Presentation of the security standards of the means

• Presentation of the type of data concerned by the service

• Document concerning the technical characteristics of the good, including the following elements:

1. Elements necessary to implement the means of cryptology:

a) 2 models of the cryptology means ;

b) the installation guides of the means;

c) activation procedures of the means, if applicable (license number, activation number, hardware device, etc.);

d) key injection or network activation devices, if applicable.

2. Elements related to cryptology algorithms:

a) description of the cryptology function offered by the means (encryption, signature, key management, etc.);

b) either the complete description of the cryptology processes used, in the form of a synoptic and mathematical description and a simulation in a high-level language;
or the reference to a previously lodged file for a means using the same cryptology methods ; or the reference to a recognized and unequivocal standard, and whose technical details are easily and unconditionally accessible, with the parameters and the operating procedures of its implementation;

c) if the encryption method implemented in the means is not a recognized standard, 3 reference outputs of the encryption method, in electronic format, from a clear text and an arbitrary chosen key, which will also be provided, in order to verify the conformity of the implementation of the process with the description thereof;

3. elements related to the management of the keys:

a) distribution mode of the keys;

b) generation process of the keys;

c) retention format of the keys;

d) transmission format of the keys.

4. The elements relating to the protection of the encryption method, namely the description of the technical measures implemented to prevent the alteration of the encryption method or the associated key management.

5. Elements relating to data processing:

a) description of pretreatments experienced by clear data before their encryption (compression, formatting, adding a header, etc.);

b) description of the post-processing of the encrypted data, after their encryption (adding a header, formatting, packaging, etc.);

c) 3 reference outputs of the means, in electronic format, made from a clear text and an arbitrary chosen key, which will also be provided, in order to verify the implementation of the means in relation to the description of this.

6. Elements relating to implementation of the cryptology:

a) the source code of the means, and the elements allowing a recompilation of the source code or the references of the associated compilers;

b) the references of the components integrating the cryptology functions of the means and the names of the manufacturers of each of these components;

c) the cryptology functions implemented by each of these components;

d) the technical documentation of the components performing the cryptological functions;

e) the types of memories (flash, ROM, EPROM, etc.) in which are stored the functions and cryptology parameters as well as the references of these memories.

7. the description of the services offered to users of the service.

8. the description of the cryptological functions implemented by the service provider.

9. the description of the premises used to implement the service.

10. the description of hardware and computer software including cryptography used by the provider.

11. the description of the physical protection and access control systems for the premises and IT systems of the service provider.

12. When the service consists of the management of cryptographic keys or electronic certificates for the benefit of users:

a) the description of the procedure for generating keys and certificates;

b) the description of the procedure for distributing and delivering keys and certificates to users;

c) the description of the technical and organizational measures implemented for the protection and preservation of keys;

d) the description of the key recovery procedure (only for the confidentiality service);

e) the references of the means of cryptology implemented by the users of the service, when these means are specifically designed to work with the keys or certificates issued by this service.