No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.0A.001

0A001

‘Nuclear reactors’ and specially designed or prepared equipment and components therefor, as follows:

a.  ‘Nuclear reactors’ capable of operation so as to maintain a controlled self-sustaining fission chain reaction;

b.  Metal vessels, or major shop-fabricated parts therefor, specially designed or prepared to contain the core of a ‘nuclear reactor’, including the reactor vessel head for a reactor pressure vessel;

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

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

e.  Pressure tubes specially designed or prepared to contain fuel elements and the primary coolant in a ‘nuclear reactor’ at an operating pressure in excess of 5,1 MPa;

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

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

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

Note: In I.0A.001.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 (steam generators) specially designed or prepared for use in the primary coolant circuit of a ‘nuclear reactor’;

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

I.0A.002

ex 0B001*

(0B001.a, 0B001.b.1-13, 0B001.c, 0B001.d 0B001.e 0B001.f 0B001.g 0B001.h 0B001.i and 0B001.j)

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

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

1.  Gas centrifuge separation plant;

2.  Gaseous diffusion separation plant;

3.  Aerodynamic separation plant;

4.  Chemical exchange separation plant;

5.  Ion-exchange separation plant;

6.  Atomic vapour ‘laser’ isotope separation (AVLIS) plant;

7.  Molecular ‘laser’ isotope separation (MLIS) plant;

8.  Plasma separation plant;

9.  Electro magnetic separation plant;

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

Note: In I.0A.002.b. ‘high strength-to-density ratio material’ means any of the following:

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

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

c.  ‘Fibrous or filamentary materials’ with a ‘specific modulus’ of more than 3,18 × 106 m and a ‘specific tensile strength’ greater than 76,2 × 103 m;

1.  Gas centrifuges;

2.  Complete rotor assemblies;

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

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

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

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

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

8.  Specially prepared bearings comprising a pivot-cup assembly mounted on a damper;

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

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

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

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

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

a.  Multiphase output of 600 to 2 000 Hz;

b.  Frequency control better than 0,1 %;

c.  Harmonic distortion of less than 2 %; and

d.  An efficiency greater than 80 %;

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

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

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

3.  Compressors (positive displacement, centrifugal and axial flow types) or gas blowers with a suction volume capacity of 1 m3/min or more of UF6, and discharge pressure up to 666,7 kPa, made of or protected by ‘materials resistant to corrosion by UF6’;

4.  Rotary shaft seals for compressors or blowers specified in I.0A.002.c.3. and designed for a buffer gas in-leakage rate of less than 1 000 cm3/min.;

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

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

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

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

2.  Tangential inlet flow-driven cylindrical or conical tubes, (vortex tubes), made of or protected by ‘materials resistant to corrosion by UF6’ with a diameter of between 0,5 cm and 4 cm and a length to diameter ratio of 20:1 or less and with one or more tangential inlets;

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

4.  Heat exchangers made of or protected by ‘materials resistant to corrosion by UF6’;

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

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

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

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

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

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

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

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

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

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

3.  Electrochemical reduction cells resistant to concentrated hydrochloric acid solutions, for reduction of uranium from one valence state to another;

4.  Electrochemical reduction cells feed equipment to take U+4 from the organic stream and, for those parts in contact with the process stream, made of or protected by suitable materials (e.g. glass, fluorocarbon polymers, polyphenyl sulphate, polyether sulfone and resin-impregnated graphite);

5.  Feed preparation systems for producing high purity uranium chloride solution consisting of dissolution, solvent extraction and/or ion exchange equipment for purification and electrolytic cells for reducing the uranium U+6 or U+4 to U+3;

6.  Uranium oxidation systems for oxidation of U+3 to U+4;

f.  Equipment and components, specially designed or prepared for ion-exchange separation process, as follows:

1.  Fast reacting ion-exchange resins, pellicular or porous macro-reticulated resins in which the active chemical exchange groups are limited to a coating on the surface of an inactive porous support structure, and other composite structures in any suitable form, including particles or fibres, with diameters of 0,2 mm or less, resistant to concentrated hydrochloric acid and designed to have an exchange rate half time of less than 10 seconds and capable of operating at temperatures in the range of 373 K (100 °C) to 473 K (200 °C);

2.  ion-exchange columns (cylindrical) with a diameter greater than 1 000 mm, made of or protected by materials resistant to concentrated hydrochloric acid (e.g. titanium or fluorocarbon plastics) and capable of operating at temperatures in the range of 373 K (100 °C) to 473 K (200 °C) and pressures above 0,7 MPa;

3.  ion-exchange reflux systems (chemical or electrochemical oxidation or reduction systems) for regeneration of the chemical reducing or oxidizing agents used in ion-exchange enrichment cascades;

g.  Equipment and components, specially designed or prepared for atomic vapour ‘laser’ isotope separation process (AVLIS), as follows:

1.  High power strip or scanning electron beam guns with a delivered power of more than 2,5 kW/cm for use in uranium vaporization systems;

2.  Liquid uranium metal handling systems for molten uranium or uranium alloys, consisting of crucibles, made of or protected by suitable corrosion and heat resistant materials (e.g. tantalum, yttria-coated graphite, graphite coated with other rare earth oxides or mixtures thereof), and cooling equipment for the crucibles;

N.B.: See also I.2A.002.

3.  Product and tails collector systems made of or lined with materials resistant to the heat and corrosion of uranium metal vapour or liquid, such as yttria-coated graphite or tantalum;

4.  Separator module housings (cylindrical or rectangular vessels) for containing the uranium metal vapour source, the electron beam gun and the product and tails collectors;

5.  ‘Lasers’ or ‘laser’ systems for the separation of uranium isotopes with a spectrum frequency stabiliser for operation over extended periods of time;

N.B.: See also I.6A.001 and I.6A.008.

h.  Equipment and components, specially designed or prepared for molecular ‘laser’ isotope separation process (MLIS) or chemical reaction by isotope selective laser activation (CRISLA), as follows:

1.  Supersonic expansion nozzles for cooling mixtures of UF6 and carrier gas to 150 K (– 123 °C) or less and made from ‘materials resistant to corrosion by UF6’;

2.  Uranium pentafluoride (UF5) product collectors consisting of filter, impact, or cyclone type collectors or combinations thereof, and made of ‘materials resistant to corrosion by UF5/UF6’;

3.  Compressors made of or protected by ‘materials resistant to corrosion by UF6’, and rotary shaft seals therefor;

4.  Equipment for fluorinating UF5 (solid) to UF6 (gas);

5.  Process systems for separating UF6 from carrier gas (e.g. nitrogen or argon) including:

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

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

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

6.  ‘Lasers’ or ‘laser’ systems for the separation of uranium isotopes with a spectrum frequency stabiliser for operation over extended periods of time;

N.B.: See also I.6A.001 and I.6A.008.

i.  Equipment and components, specially designed or prepared for plasma separation process, as follows:

1.  Microwave power sources and antennae for producing or accelerating ions, with an output frequency greater than 30 GHz and mean power output greater than 50 kW;

2.  radio-frequency ion excitation coils for frequencies of more than 100 kHz and capable of handling more than 40 kW mean power;

3.  Uranium plasma generation systems;

4.  Liquid metal handling systems for molten uranium or uranium alloys, consisting of crucibles, made of or protected by suitable corrosion and heat resistant materials (e.g. tantalum, yttria-coated graphite, graphite coated with other rare earth oxides or mixtures thereof), and cooling equipment for the crucibles;

N.B.: See also I.2A.002.

5.  Product and tails collectors made of or protected by materials resistant to the heat and corrosion of uranium vapour such as yttria-coated graphite or tantalum;

6.  Separator module housings (cylindrical) for containing the uranium plasma source, radio-frequency drive coil and the product and tails collectors and made of a suitable non-magnetic material (e.g. stainless steel);

j.  Equipment and components, specially designed or prepared for electromagnetic separation process, as follows:

1.  Ion sources, single or multiple, consisting of a vapour source, ioniser, and beam accelerator made of suitable non-magnetic materials (e.g. graphite, stainless steel, or copper) and capable of providing a total ion beam current of 50 mA or greater;

2.  Ion collector plates for collection of enriched or depleted uranium ion beams, consisting of two or more slits and pockets and made of suitable non-magnetic materials (e.g. graphite or stainless steel);

3.  Vacuum housings for uranium electromagnetic separators made of non-magnetic materials (e.g. stainless steel) and designed to operate at pressures of 0,1 Pa or lower;

4.  Magnet pole pieces with a diameter greater than 2 m;

5.  High voltage power supplies for ion sources, having all of the following characteristics:

a.  Capable of continuous operation;

b.  Output voltage of 20 000 V or greater;

c.  Output current of 1 A or greater; and

d.  Voltage regulation of better than 0,01 % over a period of 8 hours;

N.B.: See also I.3A.006.

6.  Magnet power supplies (high power, direct current) having all of the following characteristics:

a.  Capable of continuous operation with a current output of 500 A or greater at a voltage of 100 V or greater; and

b.  Current or voltage regulation better than 0,01 % over a period of 8 hours.

N.B.: See also I.3A.005.

I.0A.003

0B002

Specially designed or prepared auxiliary systems, equipment and components, as follows, for isotope separation plant specified in I.0A.002, made of or protected by ‘materials resistant to corrosion by UF6’:

a.  Feed autoclaves, ovens or systems used for passing UF6 to the enrichment process;

b.  Desublimers or cold traps, used to remove UF6 from the enrichment process for subsequent transfer upon heating;

c.  Product and tails stations for transferring UF6 into containers;

d.  Liquefaction or solidification stations used to remove UF6 from the enrichment process by compressing, cooling and converting UF6 to a liquid or solid form;

e.  Piping systems and header systems specially designed for handling UF6 within gaseous diffusion, centrifuge or aerodynamic cascades;

1.  Vacuum manifolds or vacuum headers having a suction capacity of 5 m3/minute or more; or

2.  Vacuum pumps specially designed for use in UF6 bearing atmospheres;

g.  UF6 mass spectrometers/ion sources specially designed or prepared for taking on-line samples of feed, product or tails from UF6 gas streams and having all of the following characteristics:

1.  Unit resolution for mass of more than 320 amu;

2.  Ion sources constructed of or lined with nichrome or monel, or nickel plated;

3.  Electron bombardment ionisation sources; and

4.  Collector system suitable for isotopic analysis.

I.0A.004

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.

I.0A.005

0B004

Plant for the production or concentration of heavy water, deuterium and deuterium compounds and specially designed or prepared equipment and components therefor, as follows:

a.  Plant for the production of heavy water, deuterium or deuterium compounds, as follows:

1.  Water-hydrogen sulphide exchange plants;

2.  Ammonia-hydrogen exchange plants;

b.  Equipment and components, as follows:

1.  Water-hydrogen sulphide exchange towers fabricated from fine carbon steel (e.g. ASTM A516) with diameters of 6 m to 9 m, capable of operating at pressures greater than or equal to 2 MPa and with a corrosion allowance of 6 mm or greater;

2.  Single stage, low head (i.e. 0,2 MPa) centrifugal blowers or compressors for hydrogen sulphide gas circulation (i.e. gas containing more than 70 % H2S) with a throughput capacity greater than or equal to 56 m3/second when operating at pressures greater than or equal to 1,8 MPa suction and having seals designed for wet H2S service;

3.  Ammonia-hydrogen exchange towers greater than or equal to 35 m in height with diameters of 1,5 m to 2,5 m capable of operating at pressures greater than 15 MPa;

4.  Tower internals, including stage contactors, and stage pumps, including those which are submersible, for heavy water production utilizing the ammonia-hydrogen exchange process;

5.  Ammonia crackers with operating pressures greater than or equal to 3 MPa for heavy water production utilizing the ammonia-hydrogen exchange process;

6.  Infrared absorption analysers capable of on-line hydrogen/deuterium ratio analysis where deuterium concentrations are equal to or greater than 90 %;

7.  Catalytic burners for the conversion of enriched deuterium gas into heavy water utilizing the ammonia-hydrogen exchange process;

8.  Complete heavy water upgrade systems, or columns therefor, for the upgrade of heavy water to reactor-grade deuterium concentration.

I.0A.006

0B005

Plant specially designed for the fabrication of ‘nuclear reactor’ fuel elements and specially designed or prepared equipment therefor.

Note: A plant for the fabrication of ‘nuclear reactor’ fuel elements includes equipment which:

a.  Normally comes into direct contact with or directly processes or controls the production flow of nuclear materials;

b.  Seals the nuclear materials within the cladding;

c.  Checks the integrity of the cladding or the seal; or

d.  Checks the finish treatment of the sealed fuel.

I.0A.007

0B006

Plant for the reprocessing of irradiated ‘nuclear reactor’ fuel elements, and specially designed or prepared equipment and components therefor:

Note: I.0A.007 includes:

a.  Plant for the reprocessing of irradiated ‘nuclear reactor’ fuel elements including equipment and components which normally come into direct contact with and directly control the irradiated fuel and the major nuclear material and fission product processing streams;

b.  Fuel element chopping or shredding machines, i.e. remotely operated equipment to cut, chop, shred or shear irradiated ‘nuclear reactor’ fuel assemblies, bundles or rods;

c.  Dissolvers, critically safe tanks (e.g. small diameter, annular or slab tanks) specially designed or prepared for the dissolution of irradiated ‘nuclear reactor’ fuel, which are capable of withstanding hot, highly corrosive liquids, and which can be remotely loaded and maintained;

d.  Counter-current solvent extractors and ion-exchange processing equipment specially designed or prepared for use in a plant for the reprocessing of irradiated ‘natural uranium’, ‘depleted uranium’ or ‘special fissile materials’;

e.  Holding or storage vessels specially designed to be critically safe and resistant to the corrosive effects of nitric acid;

Note: Holding or storage vessels may have the following features:

1.  Walls or internal structures with a boron equivalent (calculated for all constituent elements as defined in the note to I.0A.012) of at least two per cent;

2.  A maximum diameter of 175 mm for cylindrical vessels; or

3.  A maximum width of 75 mm for either a slab or annular vessel.

f.  Process control instrumentation specially designed or prepared for monitoring or controlling the reprocessing of irradiated ‘natural uranium’, ‘depleted uranium’ or ‘special fissile materials’.

I.0A.008

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.

I.0A.009

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: I.0A.009 does not prohibit the following:

a.  Four grammes or less of ‘natural uranium’ or ‘depleted uranium’ when contained in a sensing component in instruments;

b.  ‘Depleted uranium’ specially fabricated for the following civil non-nuclear applications:

1.  Shielding;

2.  Packaging;

3.  Ballasts having a mass not greater than 100 kg;

4.  Counter-weights having a mass not greater than 100 kg;

c.  Alloys containing less than 5 % thorium;

d.  Ceramic products containing thorium, which have been manufactured for non-nuclear use.

I.0A.010

0C002

‘Special fissile materials’.

Note: I.0A.010 does not prohibit four ‘effective grammes’ or less when contained in a sensing component in instruments.

I.0A.011

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.

I.0A.012

0C004

Graphite, nuclear grade, having a purity level of less than 5 parts per million ‘boron equivalent’ and with a density greater than 1,5 g/cm3.

N.B.: See also I.1A.028.

Note 1: I.0A.012 does not prohibit the following:

a.  Manufactures of graphite having a mass less than 1 kg, other than those specially designed or prepared for use in a nuclear reactor;

b.  Graphite powder.

Note 2: In I.0A.012, ‘boron equivalent’ (BE) is defined as the sum of BEz for impurities (excluding BEcarbon since carbon is not considered an impurity) including boron, where:

BEz (ppm) = CF × concentration of element Z in ppm;

where CF is the conversion factor =

and σB and σZ are the thermal neutron capture cross sections (in barns) for naturally occurring boron and element Z respectively; and AB and AZ are the atomic masses of naturally occurring boron and element Z respectively.

I.0A.013

0C005

Specially prepared compounds or powders for the manufacture of gaseous diffusion barriers, resistant to corrosion by UF6 (e.g. nickel or alloy containing 60 weight per cent or more nickel, aluminium oxide and fully fluorinated hydrocarbon polymers), having a purity of 99,9 weight per cent or more and a mean particle size of less than 10 micrometres measured by American Society for Testing and Materials (ASTM) B330 standard and a high degree of particle size uniformity.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.0B.001

0D001

‘Software’ specially designed or modified for the ‘development’, ‘production’ or ‘use’ of goods specified in Section I.0A.

I.0B.002

0E001

‘Technology’ according to the Nuclear Technology Note for the ‘development’, ‘production’ or ‘use’ of goods specified in Section I.0A.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.1A.001

1A102

Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

N.B.: See also Military Goods Controls for components for rockets and missiles.

I.1A.002

1A202

Composite structures in the form of tubes and having both of the following characteristics:

N.B.: See also I.9A.011.

a.  An inside diameter of between 75 mm and 400 mm; and

b.  Made with any of the ‘fibrous or filamentary materials’ specified in I.1A.024 or I.1A.034.a. or with carbon prepreg materials specified in I.1A.034.c.

I.1A.003

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.

I.1A.004

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.

I.1A.005

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 Notes:

In I.1A.005 the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application.

I.1A.006

ex 1B001*

(1B001.a, ex 1B001.b and 1B001.c)

Equipment for the production of fibres, prepregs, preforms or ‘composites’ specified in I.1A.024, as follows, and specially designed components and accessories therefor:

N.B.: See also I.1A.007 and I.1A.014.

a.  Filament winding machines of which the motions for positioning, wrapping and winding fibres are coordinated and programmed in three or more axes, specially designed for the manufacture of ‘composite’ structures or laminates from ‘fibrous or filamentary materials’;

b.*  Tape-laying machines of which the motions for positioning and laying tape or sheets are coordinated and programmed in two or more axes, specially designed for the manufacture of ‘composite’ airframe or ‘missile’ structures;

Note: In I.1A.006.b., ‘missile’ means complete rocket systems and unmanned aerial vehicle systems.

c.  Multidirectional, multidimensional weaving machines or interlacing machines, including adapters and modification kits, for weaving, interlacing or braiding fibres to manufacture ‘composite’ structures;

Technical Notes:

For the purposes of I.1A.006.c. the technique of interlacing includes knitting.

Note: I.1A.006.c. does not prohibit textile machinery not modified for the above end-uses.

I.1A.007

1B101 and ex 1B001.d

Equipment, other than that specified in I.1A.006, for the ‘production’ of structural composites as follows; and specially designed components and accessories therefor:

Note: Components and accessories specified in I.1A.007 include moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof.

a.  Filament winding machines of which the motions for positioning, wrapping and winding fibres can be coordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and coordinating and programming controls;

b.  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:

1.  Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon or polycarbosilane) including special provision to strain the fibre during heating;

2.  Equipment for the vapour deposition of elements or compounds on heated filament substrates;

3.  Equipment for the wet-spinning of refractory ceramics (such as aluminium oxide);

d.  Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms specified in entry I.9A.026.

Note: I.1A.007.d. includes rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.

I.1A.008

1B102

Metal powder ‘production equipment’ and components as follows:

N.B.: See also I.1A.009.b.

a.  Metal powder ‘production equipment’ usable for the ‘production’, in a controlled environment, of spherical or atomised materials specified in I.1A.025.a., I.1A.025.b., I.1A.029.a.1., I.1A.029.a.2. or in the Military Goods Controls.

b.  Specially designed components for ‘production equipment’ specified in I.1A.008.a.

Note: I.1A.008 includes:

a.  Plasma generators (high frequency arc-jet) usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;

b.  Electroburst equipment usable for obtaining sputtered or spherical metallic powders with organization of the process in an argon-water environment;

c.  Equipment usable for the ‘production’ of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen).

I.1A.009

1B115

Equipment, other than that specified in I.1A.008, 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 I.1A.025.a., I.1A.025.b., I.1A.029 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 I.1A.025.a., I.1A.025.b., I.1A.029 or in the Military Goods Controls.

Note: I.1A.009.b. does not prohibit batch mixers, continuous mixers or fluid energy mills. For the prohibition of batch mixers, continuous mixers and fluid energy mills see I.1A.011, I.1A.012 and I.1A.013.

Note 1: For equipment specially designed for the production of military goods, see the Military Goods Controls.

Note 2: I.1A.009 does not prohibit equipment for the ‘production’, handling and acceptance testing of boron carbide

I.1A.010

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.

I.1A.011

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.

I.1A.012

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.

I.1A.013

1B119

Fluid energy mills usable for grinding or milling substances specified in I.1A.025.a., I.1A.025.b., I.1A.029 or in the Military Goods Controls, and specially designed components therefore.

I.1A.014

1B201

Filament winding machines, other than those specified in I.1A.006 or I.1A.007, and related equipment, as follows:

a.  Filament winding machines having all of the following characteristics:

1.  Having motions for positioning, wrapping, and winding fibres coordinated and programmed in two or more axes;

2.  Specially designed to fabricate composite structures or laminates from ‘fibrous or filamentary materials’; and

3.  Capable of winding cylindrical rotors of diameter between 75 and 400 mm and lengths of 600 mm or greater;

b.  Coordinating and programming controls for the filament winding machines specified in I.1A.014.a.;

c.  Precision mandrels for the filament winding machines specified in I.1A.014.a.

I.1A.015

1B225

Electrolytic cells for fluorine production with an output capacity greater than 250 g of fluorine per hour.

I.1A.016

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: I.1A.016 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.

I.1A.017

1B227

Ammonia synthesis converters or ammonia synthesis units, in which the synthesis gas (nitrogen and hydrogen) is withdrawn from an ammonia/hydrogen high-pressure exchange column and the synthesized ammonia is returned to said column

I.1A.018

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:

1.  Stainless steel of the 300 series with low sulphur content and with an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; or

2.  Equivalent materials which are both cryogenic and H2-compatible; and

d.  With internal diameters of 1 m or greater and effective lengths of 5 m or greater.

I.1A.019

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 I.0A.005.

a.  Water-hydrogen sulphide exchange tray columns, having all of the following characteristics:

1.  Can operate at pressures of 2 MPa or greater;

2.  Constructed of carbon steel having an austenitic ASTM (or equivalent standard) grain size number of 5 or greater; and

3.  With a diameter of 1,8 m or greater;

b.  ‘Internal contactors’ for the water hydrogen sulphide exchange tray columns specified in I.1A.019.a.

Technical Notes:

‘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

I.1A.020

1B230

Pumps capable of circulating solutions of concentrated or dilute potassium amide catalyst in liquid ammonia (KNH2/NH3), having all of the following characteristics:

a.  Airtight (i.e., hermetically sealed);

b.  A capacity greater than 8,5 m3/h; and

c.  Either of the following characteristics:

1.  For concentrated potassium amide solutions (1 % or greater), an operating pressure of 1,5 to 60 MPa; or

2.  For dilute potassium amide solutions (less than 1 %), an operating pressure of 20 to 60 MPa.

I.1A.021

1B231

Tritium facilities or plants, and equipment therefor, as follows:

a.  Facilities or plants for the production, recovery, extraction, concentration, or handling of tritium;

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

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

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

I.1A.022

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.

I.1A.023

1B233

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

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

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

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

2.  Mercury or lithium amalgam pumps;

3.  Lithium amalgam electrolysis cells;

4.  Evaporators for concentrated lithium hydroxide solution.

I.1A.024

1C010.b

‘Fibrous or filamentary materials’ which may be used in organic ‘matrix’, metallic ‘matrix’ or carbon ‘matrix’‘composite’ structures or laminates, as follows:

N.B.: See also I.1A.034 and I.9A.026.

b.  Carbon ‘fibrous or filamentary materials’, having all of the following:

1.  A ‘specific modulus’ exceeding 12,7 × 106 m; and

2.  A ‘specific tensile strength’ exceeding 23,5 × 104 m;

Note: I.1A.024.b. does not prohibit fabric made from ‘fibrous or filamentary materials’ for the repair of ‘civil aircraft’ structures or laminates, in which the size of individual sheets does not exceed 100 cm × 100 cm.

Technical Notes:

Properties for materials described in I.1A.024.b. should be determined using SACMA recommended methods SRM 12 to 17, or national equivalent tow tests, such as Japanese Industrial Standard JIS-R-7601, Paragraph 6.6.2., and based on lot average.

I.1A.025

1C011.a and 1C011.b

Metals and compounds, as follows:

N.B.: See also Military Goods Controls and I.1A.029.

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 of these;

Technical Notes:

The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.

Note: The metals or alloys listed in I.1A.025.a. are prohibited whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.

b.  Boron or boron carbide of 85 % purity or higher and a particle size of 60 μm or less;

Note: The metals or alloys listed in I.1A.025.b. are prohibited whether or not the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium.

I.1A.026

1C101

Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, usable in ‘missiles’, ‘missile’ subsystems or unmanned aerial vehicles specified in I.9A.003.

Note 1: I.1A.026 includes:

a.  Structural materials and coatings specially designed for reduced radar reflectivity;

b.  Coatings, including paints, specially designed for reduced or tailored reflectivity or emissivity in the microwave, infrared or ultra violet regions of the electromagnetic spectrum.

Note 2: I.1A.026 does not include coatings when specially used for the thermal control of satellites.

Technical Notes:

In I.1A.026 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.1A.027

1C102

Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

N.B.: See also Military Goods Controls for materials for rockets and missiles.

I.1A.028

ex 1C107*

(1C107.a, ex 1C107.b, ex 1C107.c and ex 1C107.d)

Graphite and ceramic materials 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:

1.  Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater;

2.  Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or

3.  Blocks having a size of 120 mm × 120 mm × 50 mm or greater;

N.B.: See also I.0A.012.

b.*  Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in ‘missiles’;

N.B.: See also I.0A.012.

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’;

d.*  Bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips usable for ‘missiles’.

I.1A.029

ex 1C111*

(1C111.a.1-3, 1C111.a.4, 1C111.b.1-4 and 1C111.c)

Propellants and constituent chemicals for propellants, other than those specified in I.1A.025, as follows:

a.  Propulsive substances:

1.  Spherical aluminium powder, other than that specified in the Military Goods Controls, with particles of uniform diameter of less than 200 μm and an aluminium content of 97 % by weight or more, if at least 10 % of the total weight is made up of particles of less than 63 μm, according to ISO 2591:1988 or national equivalents;

Technical Notes:

A particle size of 63 μm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11).

2.  Metal fuels, other than that specified in the Military Goods Controls, in particle sizes of less than 60 μm, whether spherical, atomized, spheroidal, flaked or ground, consisting 97 % by weight or more of any of the following:

a.  Zirconium;

b.  Beryllium;

c.  Magnesium; or

d.  Alloys of the metals specified by (a) to (c) above;

Technical Notes:

The natural content of hafnium in the zirconium (typically 2 % to 7 %) is counted with the zirconium.

3.  Oxidiser substances usable in liquid propellant rocket engines as follows:

a.  Dinitrogen trioxide;

b.  Nitrogen dioxide/dinitrogen tetroxide;

c.  Dinitrogen pentoxide;

d.  Mixed Oxides of Nitrogen (MON);

Technical Notes:

Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2) that can be used in missile systems. There are a range of compositions that can be denoted as MONi or MONij, where i and j are integers representing the percentage of Nitric Oxide in the mixture (e.g., MON3 contains 3 % Nitric Oxide, MON25 25 % Nitric Oxide. An upper limit is MON40, 40 % by weight).

N.B.: See Military Goods Controls for Inhibited Red Fuming Nitric Acid (IRFNA);

N.B.: See Military Goods Controls and I.1A.049 for Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;

4.  Hydrazine derivatives as follows:

a.  trimethylhydrazine;

b.  tetramethylhydrazine;

c.  N, N diallylhydrazine;

d.  allylhydrazine;

e.  ethylene dihydrazine;

f.  monomethylhydrazine dinitrate;

g.  unsymmetrical dimethylhydrazine nitrate;

h.  hydrazinium azide;

i.  dimethylhydrazinium azide;

N.B.: See Military Goods Controls for Hydrazinium nitrate;

k.  diimido oxalic acid dihydrazine;

l.  2-hydroxyethylhydrazine nitrate (HEHN);

N.B.: See Military Goods Controls for Hydrazinium perchlorate;

n.  hydrazinium diperchlorate;

o.  methylhydrazine nitrate (MHN);

p.  diethylhydrazine nitrate (DEHN);

q.  1,4-dihydrazine nitrate (DHTN);

b.*  Polymeric substances:

1.  Carboxy-terminated polybutadiene (CTPB);

2.  Hydroxy-terminated polybutadiene (HTPB), other than that specified in the Military Goods Controls;

3.  Polybutadiene-acrylic acid (PBAA);

4.  Polybutadiene-acrylic acid-acrylonitrile (PBAN);

c.  Other propellant additives and agents:

N.B.: See Military Goods Controls for carboranes, decaboranes, pentaboranes and derivatives thereof;

2.  Triethylene glycol dinitrate (TEGDN);

3.  2-Nitrodiphenylamine (CAS 119-75-5);

4.  Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1);

5.  Diethylene glycol dinitrate (DEGDN);

6.  Ferrocene derivatives as follows:

N.B.: See Military Goods Controls for catocene;

b.  Ethyl ferrocene;

c.  Propyl ferrocene (CAS 1273-89-8);

N.B.: See Military Goods Controls for n-butyl ferrocene;

e.  Pentyl ferrocene (CAS 1274-00-6);

f.  Dicyclopentyl ferrocene;

g.  Dicyclohexyl ferrocene;

h.  Diethyl ferrocene;

i.  Dipropyl ferrocene;

j.  Dibutyl ferrocene;

k.  Dihexyl ferrocene;

l.  Acetyl ferrocenes;

N.B.: See Military Goods Controls for ferrocene Carboxylic acids;

N.B.: See Military Goods Controls for butacene;

o.  Other ferrocene derivatives usable as rocket propellant burning rate modifiers, other than those specified in the Military Goods Controls.

Note: For propellants and constituent chemicals for propellants not specified in I.1A.029, see the Military Goods Controls.

I.1A.030

1C116

Maraging steels (steels generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce age-hardening) having an ultimate tensile strength of 1 500 MPa or greater, measured at 293 K (20 °C), in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5 mm.

N.B.: See also I.1A.035.

I.1A.031

ex 1C117*

Tungsten, molybdenum and alloys of these metals in the form of uniform spherical or atomized particles of 500 micrometre diameter or less with a purity of 97 % or greater for fabrication of motor components, usable in ‘missiles’ (i.e., heat shields, nozzle substrates, nozzle throats and thrust vector control surfaces).

I.1A.032

1C118

Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following:

a.  Having all of the following characteristics:

1.  Containing 17,0-23,0 weight percent chromium and 4,5-7,0 weight percent nickel;

2.  Having a titanium content of greater than 0,10 weight percent; and

3.  A ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10 percent is austenite by volume (according to ASTM E-1181-87 or national equivalents); and

b.  Having any of the following forms:

1.  Ingots or bars having a size of 100 mm or more in each dimension;

2.  Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or

3.  Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less.

I.1A.033

1C202

Alloys as follows:

a.  Aluminium alloys having both of the following characteristics:

1.  ‘Capable of’ an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); and

2.  In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm;

b.  Titanium alloys having both of the following characteristics:

1.  ‘Capable of’ an ultimate tensile strength of 900 MPa or more at 293 K (20 °C); and

2.  In the form of tubes or cylindrical solid forms (including forgings) with an outside diameter of more than 75 mm.

Technical Notes:

The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment.

I.1A.034

1C210 and ex 1C010.a

‘Fibrous or filamentary materials’ or prepregs, other than those specified in I.1A.024, as follows:

a.  Carbon or aramid ‘fibrous or filamentary materials’ having either of the following characteristics:

1.  A ‘specific modulus’ of 12,7 × 106 m or greater; or

2.  A ‘specific tensile strength’ of 235 × 103 m or greater;

Note: I.1A.034.a. does not prohibit aramid ‘fibrous or filamentary materials’ having 0,25 percent or more by weight of an ester based fibre surface modifier;

b.  Glass ‘fibrous or filamentary materials’ having both of the following characteristics:

1.  A ‘specific modulus’ of 3,18 × 106 m or greater; and

2.  A ‘specific tensile strength’ of 76,2 × 103 m or greater;

c.  Thermoset resin impregnated continuous ‘yarns’, ‘rovings’, ‘tows’ or ‘tapes’ with a width of 15 mm or less (prepregs), made from carbon or glass ‘fibrous or filamentary materials’ specified in I.1A.024 or I.1A.034.a or .b.

Technical Notes:

The resin forms the matrix of the composite.

Note: In I.1A.034, ‘fibrous or filamentary materials’ is restricted to continuous ‘monofilaments’, ‘yarns’, ‘rovings’, ‘tows’ or ‘tapes’.

I.1A.035

1C216

Maraging steel, other than that specified in I.1A.030, ‘capable of’ an ultimate tensile strength of 2 050 MPa or more, at 293 K (20 °C).

Note: I.1A.035 does not prohibit forms in which all linear dimensions are 75 mm or less.

Technical Notes:

The phrase maraging steel ‘capable of’ encompasses maraging steel before or after heat treatment.

I.1A.036

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 I.1A.036 mixtures containing boron include boron loaded materials.

Technical Notes:

The natural isotopic abundance of boron-10 is approximately 18,5 weight per cent (20 atom per cent).

I.1A.037

1C226

Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, having both of the following characteristics:

a.  In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm; and

b.  A mass greater than 20 kg.

Note: I.1A.037 does not prohibit manufactures specially designed as weights or gamma-ray collimators

I.1A.038

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.

I.1A.039

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.

I.1A.040

1C229

Bismuth having both of the following characteristics:

a.  A purity of 99,99 % or greater by weight; and

b.  Containing less than 10 parts per million by weight of silver.

I.1A.041

1C230

Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing.

Note: I.1A.041 does not prohibit the following:

a.  Metal windows for X-ray machines, or for bore-hole logging devices;

b.  Oxide shapes in fabricated or semi-fabricated forms specially designed for electronic component parts or as substrates for electronic circuits;

c.  Beryl (silicate of beryllium and aluminium) in the form of emeralds or aquamarines.

I.1A.042

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.

I.1A.043

1C232

Helium-3 (3He), mixtures containing helium-3, and products or devices containing any of the foregoing.

Note: I.1A.043 does not prohibit a product or device containing less than 1 g of helium-3.

I.1A.044

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: I.1A.044 does not prohibit thermoluminescent dosimeters.

Technical Notes:

The natural isotopic abundance of lithium-6 is approximately 6,5 weight per cent (7,5 atom per cent).

I.1A.045

1C234

Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing.

Note: I.1A.045 does not prohibit zirconium in the form of foil having a thickness of 0,10 mm or less.

I.1A.046

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: I.1A.046 does not prohibit a product or device containing less than 1,48 × 103 GBq (40 Ci) of tritium.

I.1A.047

1C236

Alpha-emitting radionuclides having an alpha half-life of 10 days or greater but less than 200 years, in the following forms:

a.  Elemental;

b.  Compounds having a total alpha activity of 37 GBq/kg (1 Ci/kg) or greater;

c.  Mixtures having a total alpha activity of 37 GBq/kg (1 Ci/kg) or greater;

d.  Products or devices containing any of the foregoing.

Note: I.1A.047 does not prohibit a product or device containing less than 3,7 GBq (100 millicuries) of alpha activity.

I.1A.048

1C237

Radium-226 (226Ra), radium-226 alloys, radium-226 compounds, mixtures containing radium-226, manufactures therof, and products or devices containing any of the foregoing.

Note: I.1A.048 does not prohibit the following:

a.  Medical applicators;

b.  A product or device containing less than 0,37 GBq (10 millicuries) of radium-226.

I.1A.049

1C238

Chlorine trifluoride (ClF3).

I.1A.050

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.

I.1A.051

1C240

Nickel powder and porous nickel metal, other than those specified in I.0A.013, as follows:

a.  Nickel powder having both of the following characteristics:

1.  A nickel purity content of 99,0 % or greater by weight; and

2.  A mean particle size of less than 10 micrometres measured by American Society for Testing and Materials (ASTM) B330 standard;

b.  Porous nickel metal produced from materials specified in I.1A.051.a.

Note: I.1A.051 does not prohibit the following:

a.  Filamentary nickel powders;

b.  Single porous nickel sheets with an area of 1 000 cm2 per sheet or less.

Technical Notes:

I.1A.051.b. refers to porous metal formed by compacting and sintering the materials in I.1A.051.a. to form a metal material with fine pores interconnected throughout the structure.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.1B.001

ex 1D001

‘Software’ specially designed or modified for the ‘development’, ‘production’ or ‘use’ of equipment specified in I.1A.006.

I.1B.002

1D101

‘Software’ specially designed or modified for the ‘use’ of goods specified in I.1A.007 to I.1A.009, or I.1A.011 to I.1A.013.

I.1B.003

1D103

‘Software’ specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures.

I.1B.004

1D201

‘Software’ specially designed for the ‘use’ of goods specified in I.1A.014.

I.1B.005

1E001

‘Technology’ according to the General Technology Note for the ‘development’ or ‘production’ of equipment or materials specified in I.1A.006 to I.1A.051.

I.1B.006

1E101

‘Technology’ according to the General Technology Note for the ‘use’ of goods specified in I.1A.001, I.1A.006 to I.1A.013, I.1A.026, I.1A.028, I.1A.029 to I.1A.032, I.1B.002 or I.1B.003.

I.1B.007

ex 1E102

‘Technology’ according to the General Technology Note for the ‘development’ of ‘software’ specified in I.1B.001 to I.1B.003.

I.1B.008

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’.

I.1B.009

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: I.1B.009 includes ‘technology’ for the composition of precursor gases, flow-rates and process control schedules and parameters.

I.1B.010

ex 1E201

‘Technology’ according to the General Technology Note for the ‘use’ of goods specified in I.1A.002 to I.1A.005, I.1A.014 to I.1A.023, I.1A.024.b., I.1A.033 to I.1A.051, or I.1B.004.

I.1B.011

1E202

‘Technology’ according to the General Technology Note for the ‘development’ or ‘production’ of goods specified in I.1A.002 to I.1A.005.

I.1B.012

1E203

‘Technology’ according to the General Technology Note for the ‘development’ of ‘software’ specified in I.1B.004.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.2A.001

ex 2A001*

Anti-friction bearings and bearing systems, as follows, and components therefor:

Note: I.2A.001 does not prohibit balls with tolerances specified by the manufacturer in accordance with ISO 3290 as grade 5 or worse.

Radial ball bearings having all tolerances specified by the manufacturer in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or RBEC-9, or other national equivalents), or better and having all of the following characteristics:

a.  An inner ring bore diameter between 12 and 50 mm;

b.  An outer ring outside diameter between 25 and 100 mm; and

c.  A width between 10 and 20 mm.

I.2A.002

2A225

Crucibles made of materials resistant to liquid actinide metals, as follows:

a.  Crucibles having both of the following characteristics:

1.  A volume of between 150 cm3 and 8 000 cm3; and

2.  Made of or coated with any of the following materials, having a purity of 98 % or greater by weight:

a.  Calcium fluoride (CaF2);

b.  Calcium zirconate (metazirconate) (CaZrO3);

c.  Cerium sulphide (Ce2S3);

d.  Erbium oxide (erbia) (Er2O3);

e.  Hafnium oxide (hafnia) (HfO2);

f.  Magnesium oxide (MgO);

g.  Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W);

h.  Yttrium oxide (yttria) (Y2O3); or

i.  Zirconium oxide (zirconia) (ZrO2);

b.  Crucibles having both of the following characteristics:

1.  A volume of between 50 cm3 and 2 000 cm3; and

2.  Made of or lined with tantalum, having a purity of 99,9 % or greater by weight;

c.  Crucibles having all of the following characteristics:

1.  A volume of between 50 cm3 and 2 000 cm3;

2.  Made of or lined with tantalum, having a purity of 98 % or greater by weight; and

3.  Coated with tantalum carbide, nitride, boride, or any combination thereof

I.2A.003

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 Notes:

For valves with different inlet and outlet diameters, the ‘nominal size’ in I.2A.003 refers to the smallest diameter

I.2A.004

ex 2B001.a*, 2B001.d

Machine tools and any combination thereof, for removing (or cutting) metals, ceramics or ‘composites’, which, according to the manufacturer’s technical specification, can be equipped with electronic devices for ‘numerical control’, and specially designed components as follows:

N.B.: See also I.2A.016.

Note 1: I.2A.004 does not prohibit special purpose machine tools limited to the manufacture of gears.

Note 2: I.2A.004 does not prohibit special purpose machine tools limited to the manufacture of any of the following parts:

a.  Crankshafts or camshafts;

b.  Tools or cutters;

c.  Extruder worms;

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 I.2A.004.a and I.2A.016.

a.*  Machine tools for turning, for machines capable of machining diameters greater than 35 mm, having all of the following characteristics:

1.  Positioning accuracy with ‘all compensations available’ equal to or less (better) than 6 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis; and

2.  Two or more axes which can be coordinated simultaneously for ‘contouring control’;

Note 1: I.2A.004.a. does not prohibit turning machines specially designed for the production of contact lenses, having all of the following characteristics:

1.  Machine controller limited to using ophthalmic based software for part programming data input; and

2.  No vacuum chucking.

Note 2: I.2A.004.a does not prohibit bar machines (Swissturn), limited to machining only bar feed thru, if maximum bar diameter is equal to or less than 42 mm and there is no capability of mounting chucks. Machines may have drilling and/or milling capabilities for machining parts with diameters less than 42 mm.

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’;

I.2A.005

ex 2B006.b*

Dimensional inspection or measuring systems, equipment and ‘electronic assemblies’, as follows:

b.*  Linear and angular displacement measuring instruments, as follows:

1.*  Linear displacement measuring instruments having any of the following:

Technical Notes:

For the purpose of I.2A.005.b.1. ‘linear displacement’ means the change of distance between the measuring probe and the measured object.

a.  Non-contact type measuring systems with a ‘resolution’ equal to or less (better) than 0,2 μm within a measuring range up to 0,2 mm;

b.  Linear voltage differential transformer systems having all of the following characteristics:

1.  ‘Linearity’ equal to or less (better) than 0,1 % within a measuring range up to 5 mm; and

2.  Drift equal to or less (better) than 0,1 % per day at a standard ambient test room temperature ± 1 K; or

c.  Measuring systems having all of the following:

1.  Containing a ‘laser’; and

2.  Maintaining, for at least 12 hours, over a temperature range of ± 1 K around a standard temperature and at a standard pressure, all of the following:

a.  A ‘resolution’ over their full scale of 0,1 μm or less (better); and

b.  A ‘measurement uncertainty’ equal to or less (better) than (0,2 + L/2 000) μm (L is the measured length in mm);

Note: I.2A.005.b.1.c does not prohibit measuring interferometer systems, without closed or open loop feedback, containing a laser to measure slide movement errors of machine tools, dimensional inspection machines, or similar equipment.

2.  Angular displacement measuring instruments having an ‘angular position deviation’ equal to or less (better) than 0,00025 °;

Note: I.2A.005.b.2. does not prohibit optical instruments, such as autocollimators, using collimated light (e.g. laser light) to detect angular displacement of a mirror

I.2A.006

2B007.c

‘Robots’ having the following characteristics and specially designed controllers and ‘end-effectors’ therefor:

N.B.: See also I.2A.019.

c.  Specially designed or rated as radiation-hardened to withstand a total radiation dose greater than 5 × 103 Gy (silicon) without operational degradation.

Technical Notes:

The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation.

I.2A.007

2B104

‘Isostatic presses’ having all of the following:

N.B.: See also I.2A.017.

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.

I.2A.008

2B105

Chemical vapour deposition (CVD) furnaces designed or modified for the densification of carbon-carbon composites.

I.2A.009

2B109

Flow-forming machines and specially designed components as follows:

N.B.: See also I.2A.020.

a.  Flow-forming machines having all of the following:

1.  According to the manufacturer's technical specification, can be equipped with ‘numerical control’ units or a computer control, even when not equipped with such units; and

2.  With more than two axes which can be coordinated simultaneously for ‘contouring control’.

b.  Specially designed components for flow-forming machines specified in I.2A.009.a.

Note: I.2A.009 does not prohibit machines that are not usable in the production of propulsion components and equipment (e.g. motor cases) for ‘missiles’.

Technical Notes:

Machines combining the function of spin-forming and flow-forming are for the purpose of I.2A.009 regarded as flow-forming machines

I.2A.010

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 and 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 bandwidth’ greater than 5 kHz designed for use with vibration test systems specified in I.2A.010.a.;

c.  Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured ‘bare table’, and usable in vibration test systems specified in I.2A.010.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 I.2A.010.a.

Technical Notes:

In I.2A.010, ‘bare table’ means a flat table, or surface, with no fixture or fittings

I.2A.011

2B117

Equipment and process controls, other than those specified in I.2A.007 or I.2A.008, designed or modified for densification and pyrolysis of structural composite rocket nozzles and reentry vehicle nose tips.

I.2A.012

2B119

Balancing machines and related equipment, as follows:

N.B.: See also I.2A.021.

a.  Balancing machines having all the following characteristics:

1.  Not capable of balancing rotors/assemblies having a mass greater than 3 kg;

2.  Capable of balancing rotors/assemblies at speeds greater than 12 500 rpm;

3.  Capable of correcting unbalance in two planes or more; and

4.  Capable of balancing to a residual specific unbalance of 0,2 g mm per kg of rotor mass;

Note: I.2A.012.a. does not prohibit balancing machines designed or modified for dental or other medical equipment.

b.  Indicator heads designed or modified for use with machines specified in I.2A.012.a.

Technical Notes:

Indicator heads are sometimes known as balancing instrumentation

I.2A.013

2B120

Motion simulators or rate tables having all of the following characteristics:

a.  Two axes or more;

b.  Slip rings capable of transmitting electrical power and/or signal information; and

c.  Having any of the following characteristics:

1.  For any single axis having all of the following:

a.  Capable of rates of 400 degrees/s or more, or 30 degrees/s or less; and

b.  A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0,6 degrees/s;

2.  Having a worst-case rate stability equal to or better (less) than plus or minus 0,05 % averaged over 10 degrees or more; or

3.  A positioning accuracy equal to or better than 5 arc second.

Note: I.2A.013 does not prohibit rotary tables designed or modified for machine tools or for medical equipment.

I.2A.014

2B121

Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in I.2A.013, having all the following characteristics:

a.  Two axes or more; and

b.  A positioning accuracy equal to or better than 5 arc second.

Note: I.2A.014 does not prohibit rotary tables designed or modified for machine tools or for medical equipment.

I.2A.015

2B122

Centrifuges capable of imparting accelerations above 100 g and having slip rings capable of transmitting electrical power and signal information.

I.2A.016

2B201, 2B001.b.2 and 2B001.c.2

Machine tools and any combination thereof, 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:

Note: For ‘numerical control’ units prohibited because of their associated ‘software’ see I.2B.002.

a.  Machine tools for milling, having any of the following characteristics:

1.  Positioning accuracies with ‘all compensations available’ equal to or less (better) than 6 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis;

2.  Two or more contouring rotary axes; or

3.  Five or more axes which can be coordinated simultaneously for ‘contouring control’.

Note: I.2A.016.a. does not prohibit milling machines having the following characteristics:

a.  X-axis travel greater than 2 m; and

b.  Overall positioning accuracy on the x-axis more (worse) than 30 μm.

b.  Machine tools for grinding, having any of the following characteristics:

1.  Positioning accuracies with ‘all compensations available’ equal to or less (better) than 4 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis;

2.  Two or more contouring rotary axes; or

3.  Five or more axes which can be coordinated simultaneously for ‘contouring control’.

Note: I.2A.016.b. does not prohibit the following grinding machines:

a.  Cylindrical external, internal, and external-internal grinding machines having all of the following characteristics:

1.  Limited to a maximum workpiece capacity of 150 mm outside diameter or length; and

2.  Axes limited to x, z and c;

b.  Jig grinders that do not have a z-axis or a w-axis with an overall positioning accuracy less (better) than 4 μm according to ISO 230/2 (1988) (1) or national equivalents.

Note 1: I.2A.016 does not prohibit special purpose machine tools limited to the manufacture of any of the following parts:

a.  Gears;

b.  Crankshafts or camshafts;

c.  Tools or cutters;

d.  Extruder worms.

Note 2: A machine tool having at least two of the three turning, milling or grinding capabilities (e.g., a turning machine with milling capability), must be evaluated against each applicable entry I.2A.004.a. or I.2A.016.a. or b.

I.2A.017

2B204

‘Isostatic presses’, other than those specified in I.2A.007, and related equipment, as follows:

a.  ‘Isostatic presses’ having both of the following characteristics:

1.  Capable of achieving a maximum working pressure of 69 MPa or greater; and

2.  A chamber cavity with an inside diameter in excess of 152 mm;

b.  Dies, moulds and controls, specially designed for ‘isostatic presses’ specified in I.2A.017.a.

Technical Notes:

In I.2A.017 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.

I.2A.018

2B206

Dimensional inspection machines, instruments or systems, other than those specified in I.2A.005, as follows:

a.  Computer controlled or numerically controlled dimensional inspection machines having both of the following characteristics:

1.  Two or more axes; and

2.  A one-dimensional length ‘measurement uncertainty’ equal to or less (better) than (1,25 + L/1 000) μm tested with a probe of an ‘accuracy’ of less (better) than 0,2 μm (L is the measured length in millimetres) (Ref.: VDI/VDE 2617 Parts 1 and 2);

b.  Systems for simultaneous linear-angular inspection of hemishells, having both of the following characteristics:

1.  ‘Measurement uncertainty’ along any linear axis equal to or less (better) than 3,5 μm per 5 mm; and

2.  ‘Angular position deviation’ equal to or less than 0,02 °.

Note 1: Machine tools that can be used as measuring machines are prohibited if they meet or exceed the criteria specified for the machine tool function or the measuring machine function.

Note 2: A machine specified in I.2A.018 is prohibited if it exceeds the prohibition threshold anywhere within its operating range.

1.  The probe used in determining the measurement uncertainty of a dimensional inspection system shall be described in VDI/VDE 2617 parts 2, 3 and 4.

2.  All parameters of measurement values in I.2A.018 represent plus/minus i.e., not total band.

I.2A.019

2B207

‘Robots’, ‘end-effectors’ and control units, other than those specified in I.2A.006, 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 I.2A.019.a.

I.2A.020

2B209

Flow forming machines, spin forming machines capable of flow forming functions, other than those specified in I.2A.009, and mandrels, as follows:

a.  Machines having both of the following characteristics:

1.  Three or more rollers (active or guiding); and

2.  Which, according to the manufacturer's technical specification, can be equipped with ‘numerical control’ units or a computer control;

b.  Rotor-forming mandrels designed to form cylindrical rotors of inside diameter between 75 mm and 400 mm.

Note: I.2A.020.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.

I.2A.021

2B219

Centrifugal multiplane balancing machines, fixed or portable, horizontal or vertical, as follows:

a.  Centrifugal balancing machines designed for balancing flexible rotors having a length of 600 mm or more and having all of the following characteristics:

1.  Swing or journal diameter greater than 75 mm;

2.  Mass capability of from 0,9 to 23 kg; and

3.  Capable of balancing speed of revolution greater than 5 000 r.p.m.;

b.  Centrifugal balancing machines designed for balancing hollow cylindrical rotor components and having all of the following characteristics:

1.  Journal diameter greater than 75 mm;

2.  Mass capability of from 0,9 to 23 kg;

3.  Capable of balancing to a residual imbalance equal to or less than 0,01 kg × mm/kg per plane; and

4.  Belt drive type.

I.2A.022

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 Notes:

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.

I.2A.023

2B226

Controlled atmosphere (vacuum or inert gas) induction furnaces, and power supplies therefor, as follows:

a.  Furnaces having all of the following characteristics:

1.  Capable of operation above 1 123 K (850 °C);

2.  Induction coils 600 mm or less in diameter; and

3.  Designed for power inputs of 5 kW or more;

b.  Power supplies, with a specified power output of 5 kW or more, specially designed for furnaces specified in I.2A.023.a.

Note: I.2A.023.a. does not prohibit furnaces designed for the processing of semiconductor wafers.

I.2A.024

2B227

Vacuum or other controlled atmosphere metallurgical melting and casting furnaces and related equipment as follows:

a.  Arc remelt and casting furnaces having both of the following characteristics:

1.  Consumable electrode capacities between 1 000 cm3 and 20 000 cm3, and

2.  Capable of operating with melting temperatures above 1 973 K (1 700 °C);

b.  Electron beam melting furnaces and plasma atomization and melting furnaces, having both of the following characteristics:

1.  A power of 50 kW or greater; and

2.  Capable of operating with melting temperatures above 1 473 K (1 200 °C);

c.  Computer control and monitoring systems specially configured for any of the furnaces specified in I.2A.024.a. or b.

I.2A.025

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;

Note: I.2A.025.a. includes precision mandrels, clamps, and shrink fit machines.

b.  Rotor straightening equipment for alignment of gas centrifuge rotor tube sections to a common axis;

Technical Notes:

In I.2A.025.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 Notes:

In I.2A.025.c. the bellows have all of the following characteristics:

1.  Inside diameter between 75 mm and 400 mm;

2.  Length equal to or greater than 12,7 mm;

3.  Single convolution depth greater than 2 mm; and

4.  Made of high-strength aluminium alloys, maraging steel or high strength ‘fibrous or filamentary materials’.

I.2A.026

2B230

‘Pressure transducers’ capable of measuring absolute pressures at any point in the range 0 to 13 kPa and having both of the following characteristics:

a.  Pressure sensing elements made of or protected by aluminium, aluminium alloy, nickel or nickel alloy with more than 60 % nickel by weight; and

b.  Having either of the following characteristics:

1.  A full scale of less than 13 kPa and an ‘accuracy’ of better than + 1 % of full scale; or

2.  A full scale of 13 kPa or greater and an ‘accuracy’ of better than + 130 Pa.

Technical Notes:

For the purposes of I.2A.026, ‘accuracy’ includes non-linearity, hysteresis and repeatability at ambient temperature.

I.2A.027

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.

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

I.2A.028

2B232

Multistage light gas guns or other high-velocity gun systems (coil, electromagnetic, and electrothermal types, and other advanced systems) capable of accelerating projectiles to 2 km/s or greater

(1)   Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) should consult the competent authorities of the Member State in which they are established.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.2B.001

ex 2D001

‘Software’, other than that specified in I.2B.002, specially designed or modified for the ‘development’, ‘production’ or ‘use’ of equipment specified in I.2A.004 to I.2A.006.

I.2B.002

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: I.2B.002 does not prohibit ‘software’ specially designed or modified for the operation of machine tools not specified in Category I.2.

I.2B.003

2D101

‘Software’ specially designed or modified for the ‘use’ of equipment specified in I.2A.007 to I.2A.015.

I.2B.004

2D201

‘Software’ specially designed for the ‘use’ of equipment specified in I.2A.017 to I.2A.024.

Note:‘Software’ specially designed for equipment specified in I.2A.018 includes ‘software’ for simultaneous measurements of wall thickness and contour

I.2B.005

2D202

‘Software’ specially designed or modified for the ‘development’, ‘production’ or ‘use’ of equipment specified in I.2A.016.

I.2B.006

ex 2E001

‘Technology’ according to the General Technology Note for the ‘development’ of equipment or ‘software’ specified in I.2A.002 to I.2A.004, I.2A.006.b., I.2A.006.c, I.2A.007 to I.2A.028, I.2B.001, I.2B.003 or I.2B.004.

I.2B.007

ex 2E002

‘Technology’ according to the General Technology Note for the ‘production’ of equipment specified in I.2A.002 to I.2A.004, I.2A.006.b., I.2A.006.c, I.2A.007 to I.2A.028.

I.2B.008

2E101

‘Technology’ according to the General Technology Note for the ‘use’ of equipment or ‘software’ specified in I.2A.007, I.2A.009, I.2A.010, I.2A.012 to I.2A.015 or I.2B.003.

I.2B.009

ex 2E201

‘Technology’ according to the General Technology Note for the ‘use’ of equipment or ‘software’ specified in I.2A.002 to I.2A.005, I.2A.006.b., I.2A.006.c., I.2A.016 to I.2A.020, I.2A.022 to I.2A.028, I.2B.004 or I.2B.005.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.3A.001

ex 3A001.a*

Electronic components, as follows:

a.  General purpose integrated circuits, as follows:

Note 1: The prohibition status of wafers (finished or unfinished), in which the function has been determined, is to be evaluated against the parameters of I.3A.001.a.

Note 2: Integrated circuits include the following types:

‘Monolithic integrated circuits’;

‘Hybrid integrated circuits’;

‘Multichip integrated circuits’;

‘Film type integrated circuits’, including silicon-on-sapphire integrated circuits;

‘Optical integrated circuits’.

1.*  Integrated circuits having all of the following characteristics:

a.  Designed or rated as radiation hardened to withstand a total irradiation dose of 5 × 103 Gy (silicon) or higher; and

b.  Usable in protecting rocket systems and ‘unmanned aerial vehicles’ against nuclear effects (e.g., Electromagnetic Pulse (EMP), X-rays, combined blast and thermal effects), and usable for ‘missiles’.

I.3A.002

3A101

Electronic equipment, devices and components, 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.

Note: I.3A.002.b. above does not specify equipment specially designed for medical purposes.

I.3A.003

3A201

Electronic components as follows;

a.  Capacitors having either of the following sets of characteristics:

a.  Voltage rating greater than 1,4 kV;

b.  Energy storage greater than 10 J;

c.  Capacitance greater than 0,5 μF; and

d.  Series inductance less than 50 nH; or

a.  Voltage rating greater than 750 V;

b.  Capacitance greater than 0,25 μF; and

c.  Series inductance less than 10 nH;

b.  Superconducting solenoidal electromagnets having all of the following characteristics:

1.  Capable of creating magnetic fields greater than 2 T;

2.  A ratio of length to inner diameter greater than 2;

3.  Inner diameter greater than 300 mm; and

4.  Magnetic field uniform to better than 1 % over the central 50 % of the inner volume;

Note: I.3A.003.b. does not prohibit magnets specially designed for and exported ‘as parts of’ medical nuclear magnetic resonance (NMR) imaging systems. The phrase ‘as part of’ does not necessarily mean physical part in the same shipment; separate shipments from different sources are allowed, provided the related export documents clearly specify that the shipments are dispatched ‘as part of’ the imaging systems.

c.  Flash X-ray generators or pulsed electron accelerators having either of the following sets of characteristics:

a.  An accelerator peak electron energy of 500 keV or greater but less than 25 MeV; and

b.  With a ‘figure of merit’ (K) of 0,25 or greater; or

a.  An accelerator peak electron energy of 25 MeV or greater; and

b.  A ‘peak power’ greater than 50 MW.

Note: I.3A.003.c. does not prohibit accelerators that are component parts of devices designed for purposes other than electron beam or X-ray radiation (electron microscopy, for example) nor those designed for medical purposes:

1.  The ‘figure of merit’ K is defined as:

K = 1,7 × 103V2,.65Q

V is the peak electron energy in million electron volts.

If the accelerator beam pulse duration is less than or equal to 1 μs, then Q is the total accelerated charge in Coulombs. If the accelerator beam pulse duration is greater than 1 μs, then Q is the maximum accelerated charge in 1 μs.

Q equals the integral of i with respect to t, over the lesser of 1 μs or the time duration of the beam pulse (Q = ∫ idt), where i is beam current in amperes and t is time in seconds.

2.  ‘Peak power’ = (peak potential in volts) × (peak beam current in amperes).

3.  In machines based on microwave accelerating cavities, the time duration of the beam pulse is the lesser of 1 μs or the duration of the bunched beam packet resulting from one microwave modulator pulse.

4.  In machines based on microwave accelerating cavities, the peak beam current is the average current in the time duration of a bunched beam packet

I.3A.004

3A225

Frequency changers or generators, other than those specified in I.0A.002.b.13., having all of the following characteristics:

a.  Multiphase output capable of providing a power of 40 W or greater;

b.  Capable of operating in the frequency range between 600 and 2 000 Hz;

c.  Total harmonic distortion better (less) than 10 %; and

d.  Frequency control better (less) than 0,1 %.

Technical Notes:

Frequency changers in I.3A.004 are also known as converters or inverters.

I.3A.005

3A226

High-power direct current power supplies, other than those specified in I.0A.002.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

I.3A.006

3A227

High-voltage direct current power supplies, other than those specified in I.0A.002.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.

I.3A.007

3A228

Switching devices, as follows:

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

1.  Containing three or more electrodes;

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

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

4.  Anode delay time of 10 μs or less;

Note: I.3A.007 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;

c.  Modules or assemblies with a fast switching function having all of the following characteristics:

1.  Anode peak voltage rating greater than 2 kV;

2.  Anode peak current rating of 500 A or more; and

3.  Turn on time of 1 μs or less.

I.3A.008

3A229

Firing sets and equivalent high-current pulse generators as follows:

N.B.: See also Military Goods Controls.

a.  Explosive detonator firing sets designed to drive multiple controlled detonators specified in I.3A.011;

b.  Modular electrical pulse generators (pulsers) having all of the following characteristics:

1.  Designed for portable, mobile, or ruggedized-use;

2.  Enclosed in a dust-tight enclosure;

3.  Capable of delivering their energy in less than 15 μs;

4.  Having an output greater than 100 A;

5.  Having a ‘rise time’ of less than 10 μs into loads of less than 40 ohms;

6.  No dimension greater than 254 mm;

7.  Weight less than 25 kg; and

8.  Specified for use over an extended temperature range 223 K (– 50 °C) to 373 K (100 °C) or specified as suitable for aerospace applications.

Note: I.3A.008.b. includes xenon flash lamp drivers.

Technical Notes:

In I.3A.008.b.5. ‘rise time’ is defined as the time interval from 10 % to 90 % current amplitude when driving a resistive load

I.3A.009

3A230

High-speed pulse generators having both of the following characteristics:

a.  Output voltage greater than 6 V into a resistive load of less than 55 ohms, and

b.  ‘Pulse transition time’ less than 500 ps.

Technical Note:

In I.3A.009, ‘pulse transition time’ is defined as the time interval between 10 % and 90 % voltage amplitude

I.3A.010

3A231

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

a.  Designed for operation without an external vacuum system; and

b.  Utilizing electrostatic acceleration to induce a tritium-deuterium nuclear reaction

I.3A.011

3A232

Detonators and multipoint initiation systems, as follows:

N.B.: See also Military Goods Controls.

a.  Electrically driven explosive detonators, as follows:

1.  Exploding bridge (EB);

2.  Exploding bridge wire (EBW);

3.  Slapper;

4.  Exploding foil initiators (EFI);

b.  Arrangements using single or multiple detonators designed to nearly simultaneously initiate an explosive surface over greater than 5 000 mm2 from a single firing signal with an initiation timing spread over the surface of less than 2,5 μs.

Note: I.3A.011 does not prohibit detonators using only primary explosives, such as lead azide.

Technical Note:

In I.3A.011 the detonators of concern all utilise a small electrical conductor (bridge, bridge wire or foil) that explosively vapourises when a fast, high-current electrical pulse is passed through it. In nonslapper-types, the exploding conductor starts a chemical detonation in a contacting high-explosive material such as PETN (Pentaerythritoltetranitrate). In slapper detonators, the explosive vapourisation 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 a magnetic force. The term exploding foil detonator may refer to either an EB or a slapper-type detonator. Also, the word initiator is sometimes used in place of the word detonator

I.3A.012

3A233

Mass spectrometers, other than those specified in I.0A.002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor:

a.  Inductively coupled plasma mass spectrometers (ICP/MS);

b.  Glow discharge mass spectrometers (GDMS);

c.  Thermal ionization mass spectrometers (TIMS);

d.  Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with materials resistant to UF6;

e.  Molecular beam mass spectrometers having either of the following characteristics:

1.  A source chamber constructed from, lined with or plated with stainless steel or molybdenum and equipped with a cold trap capable of cooling to 193 K (– 80 °C) or less; or

2.  A source chamber constructed from, lined with or plated with materials resistant to UF6;

f.  Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.3B.001

3D101

‘Software’ specially designed or modified for the ‘use’ of equipment specified in I.3A.002.b

I.3B.002

ex 3E001

‘Technology’ according to the General Technology Note for the ‘development’ or ‘production’ of equipment or materials specified in I.3A.001 to I.3A.003, or in I.3A.007 to I.3A.012.

I.3B.003

ex 3E101

‘Technology’ according to the General Technology Note for the ‘use’ of equipment or ‘software’ specified in I.3A.001, I.3A.002 or I.3B.001.

I.3B.004

3E102

‘Technology’ according to the General Technology Note for the ‘development’ of ‘software’ specified in I.3B.001.

I.3B.005

ex 3E201

‘Technology’ according to the General Technology Note for the ‘use’ of equipment specified in I.3A.003 to I.3A.012.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.4A.001

4A001.a.1 *

Electronic computers and related equipment, as follows:

N.B.: See also I.4A.002.

a.  Specially designed to have the following characteristics:

1.*  Rated for continuous operation at temperatures below 228 K (– 45 °C) or above 328 K (55 °C);

Note: I.4A.001 does not apply to computers specially designed for civil automobile or railway train applications.

I.4A.002

4A101*

Analogue computers, ‘digital computers’ or digital differential analysers having all of the following characteristics:

N.B.: See also Military Goods Controls for computers for use in rockets or missiles.

a.  Designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005; and

b.  Designed as ruggedised or radiation hardened to withstand radiation levels of 5 × 103 Gy (silicon) or higher.

I.4A.003

4A102

‘Hybrid computers’ specially designed for modelling, simulation or design integration of space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

N.B.: See also Military Goods Controls for rockets or missiles related computers.

Note: This prohibition only applies when the equipment is supplied with ‘software’ specified in I.7B.003 or I.9B.003.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.4B.001

ex 4E001.a

‘Technology’ according to the General Technology Note, for the ‘development’, ‘production’ or ‘use’ of equipment or ‘software’ specified in I.4A.001, I.4A.002 or I.4A.003.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.5A.001

5A101

Telemetering and telecontrol equipment, including ground equipment, designed or modified for ‘missiles’.

Technical Notes:

In I.5A.001 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

Note:I.5A.001 does not prohibit:

a.  Equipment designed or modified for manned aircraft or satellites;

b.  Ground based equipment designed or modified for terrestrial or marine applications;

c.  Equipment designed for commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) GNSS services;

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.5B.001

5D101

‘Software’ specially designed or modified for the ‘use’ of equipment specified in I.5A.001.

I.5B.002

5E101

‘Technology’ according to the General Technology Note for the ‘development’, ‘production’ or ‘use’ of equipment specified in I.5A.001 or software specified in I.5B.001.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.6A.001

ex 6A005.b*, ex 6A005.c* and ex 6A005.d*

a.:

ex 6A005.d.4

b.:

ex 6A005.b.2-4

c.:

ex 6A005.c.2

‘Lasers’, other than those specified in I.0A.002.g.5. or I.0A.002.h.6., components and optical equipment, as follows: (1)

a. (1)  Pulsed excimer (XeF, XeCl, KrF) ‘lasers’ having all of the following characteristics:

1.  Operating at wavelengths between 240 nm and 360 nm;

2.  A repetition rate greater than 250 Hz; and

3.  An average output power exceeding 500 W.

b. (1)  Copper (Cu) vapour ‘lasers’ having both of the following characteristics:

1.  Operating at wavelengths between 500 nm and 600 nm; and

2.  An average output power exceeding 40 W.

c. (1)  Solid state ‘tunable’ alexandrite (CR: BeAl2O4) ‘lasers’ having all of the following characteristics:

1.  Operating at wavelengths between 720 nm and 800 nm;

2.  A bandwidth of 0,005 nm or less;

3.  A repetition rate greater than 125 Hz; and

4.  An average output power exceeding 30 W.

I.6A.002

6A007.c

Gravity gradiometers.

I.6A.003

6A102

Radiation hardened ‘detectors’ 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 Notes:

In I.6A.003, 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.

I.6A.004

6A107

Gravity meters (gravimeters) and components for gravity meters and gravity gradiometers, as follows:

a.  Gravity meters, designed or modified for airborne or marine use, and having a static or operational accuracy of 7 × 10-6 m/s2 (0,7 milligal) or less (better), and having a time-to-steady-state registration of two minutes or less;

b.  Specially designed components for gravity meters specified in I.6A.004.a. and gravity gradiometers specified in I.6A.002.

I.6A.005

6A108

Radar systems and tracking systems as follows:

a.  Radar and laser radar systems designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005;

N.B.: See also Military Goods Controls for radar and laser systems for rockets or missiles.

Note: I.6A.005.a. includes the following:

a.  Terrain contour mapping equipment;

b.  Imaging sensor equipment;

c.  Scene mapping and correlation (both digital and analogue) equipment;

d.  Doppler navigation radar equipment.

b.  Precision tracking systems, usable for ‘missiles’, as follows:

1.  Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity;

2.  Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:

a.  Angular resolution better than 3 milliradians;

b.  Range of 30 km or greater with a range resolution better than 10 m rms;

c.  Velocity resolution better than 3 m/s.

Technical Notes:

In I.6A.005.b. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.6A.006

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.

I.6A.007

6A203

Cameras and components, as follows:

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

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

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

Note: In I.6A.007.a. components of such cameras include their synchronizing electronics units and rotor assemblies consisting of turbines, mirrors and bearings.

b.  Electronic streak cameras, electronic framing cameras, tubes and devices, as follows:

1.  Electronic streak cameras capable of 50 ns or less time resolution;

2.  Streak tubes for cameras specified in I.6A.007.b.1.;

3.  Electronic (or electronically shuttered) framing cameras capable of 50 ns or less frame exposure time;

4.  Framing tubes and solid-state imaging devices for use with cameras specified in I.6A.007.b.3., as follows:

a.  Proximity focused image intensifier tubes having the photocathode deposited on a transparent conductive coating to decrease photocathode sheet resistance;

b.  Gate silicon intensifier target (SIT) videcon tubes, where a fast system allows gating the photoelectrons from the photocathode before they impinge on the SIT plate;

c.  Kerr or Pockels cell electro-optical shuttering;

d.  Other framing tubes and solid-state imaging devices having a fast-image gating time of less than 50 ns specially designed for cameras specified in I.6A.007.b.3.;

c.  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 Notes:

The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation

I.6A.008

6A205

‘Lasers’, ‘laser’ amplifiers and oscillators, other than those specified in I.0A.002.g.5., I.0A.002.h.6. and I.6A.001; as follows:

a.  Argon ion ‘lasers’ having both of the following characteristics:

1.  Operating at wavelengths between 400 nm and 515 nm; and

2.  An average output power greater than 40 W;

b.  Tunable pulsed single-mode dye laser oscillators having all of the following characteristics:

1.  Operating at wavelengths between 300 nm and 800 nm;

2.  An average output power greater than 1 W;

3.  A repetition rate greater than 1 kHz; and

4.  Pulse width less than 100 ns;

c.  Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:

1.  Operating at wavelengths between 300 nm and 800 nm;

2.  An average output power greater than 30 W;

3.  A repetition rate greater than 1 kHz; and

4.  Pulse width less than 100 ns;

Note: I.6A.008.c. does not prohibit single mode oscillators;

d.  Pulsed carbon dioxide ‘lasers’ having all of the following characteristics:

1.  Operating at wavelengths between 9 000 nm and 11 000 nm;

2.  A repetition rate greater than 250 Hz;

3.  An average output power greater than 500 W; and

4.  Pulse width of less than 200 ns;

e.  Para-hydrogen Raman shifters designed to operate at 16 micrometre output wavelength and at a repetition rate greater than 250 Hz;

f.  Neodymium-doped (other than glass) ‘lasers’, having an output wavelength exceeding 1 000 nm but not exceeding 1 100 nm, as follows:

1.  Pulse-excited, ‘Q-switched lasers’ having a ‘pulse duration’ equal to or more than 1 ns, and having either of the following:

a.  A single-transverse mode output having an average output power exceeding 40 W; or

b.  A multiple-transverse mode output having an average power exceeding 50 W; or

2.  Incorporating frequency doubling to give an output wavelength of 500 nm or more but not exceeding 550 nm and having an average output power exceeding 40 W.

I.6A.009

6A225

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

Note: I.6A.009 includes velocity interferometers such as VISARs (Velocity interferometer systems for any reflector) and DLIs (Doppler laser interferometers).

I.6A.010

6A226

Pressure sensors, as follows:

a.  Manganin gauges for pressures greater than 10 GPa;

b.  Quartz pressure transducers for pressures greater than 10 GPa

I.6A.011

ex 6B108*

Systems specially designed for radar cross section measurement usable for ‘missiles’ and their subsystems.

(1)   The texts of points a, b and c in this entry do not correspond with those of points a, b and c of 6A005.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.6B.001

6D102

‘Software’ specially designed or modified for the ‘use’ of goods specified in I.6A.005.

I.6B.002

6D103

‘Software’ which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for ‘missiles’.

Technical Notes:

In I.6B.002 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.6B.003

ex 6E001

‘Technology’ according to the General Technology Note for the ‘development’ of equipment, materials or ‘software’ specified in I.6A.001, I.6A.002.c, I.6A.003, I.6A.004 to I.6A.010, I.6B.001 or I.6B.002.

I.6B.004

ex 6E002

‘Technology’ according to the General Technology Note for the ‘production’ of equipment or materials specified in I.6A.001, I.6A.002.c or I.6A.003 to I.6A.010.

I.6B.005

ex 6E101

‘Technology’ according to the General Technology Note for the ‘use’ of equipment or ‘software’ specified in I.6A.002 to I.6A.005, I.6A.011, I.6B.001 or I.6B.002.

I.6B.006

ex 6E201

‘Technology’ according to the General Technology Note for the ‘use’ of equipment specified in I.6A.001 or I.6A.006 to I.6A.010.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.7A.001

ex 7A002*

(ex 7A002.a and ex 7A002.d)

Gyros having any of the following characteristics, and specially designed components therefor:

N.B.: See also I.7A.003.

a.  A ‘drift rate’‘stability’, when measured in a 1 g environment over a period of one month and with respect to a fixed calibration value, of less (better) than 0,5 degree per hour when specified to function at linear acceleration levels up to and including 100 g; or

b.  Specified to function at linear acceleration levels exceeding 100 g.

I.7A.002

7A101, ex 7A001.a.3

Accelerometers as follows, and specially designed components therefor:

a.  Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in ‘missiles’, having all the following characteristics, and specially designed components therefor;

1.  A ‘bias’‘repeatability’ of less (better) than 1 250 micro g; and

2.  A ‘scale factor’‘repeatability’ of less (better) than 1 250 ppm;

Note: I.7A.002.a. does not specify accelerometers which are specially designed and developed as MWD (Measurement While Drilling) Sensors for use in downhole well service operations.

1.  In I.7A.002.a. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km;

2.  In I.7A.002.a. the measurement of ‘bias’ and ‘scale factor’ refers to a one sigma standard deviation with respect to a fixed calibration over a period of one year;

b.  Continuous output accelerometers specified to function at acceleration levels exceeding 100 g.

I.7A.003

7A102*

All types of gyros, other than those specified in I.7A.001, 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 Note:

In I.7A.003 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.7A.004

ex 7A103

(7A103.a, ex 7A103.b and 7A103.c)

Instrumentation, navigation equipment and systems, as follows; and specially designed components therefor:

a.*  Inertial or other equipment using accelerometers specified in I.7A.002 or gyros specified in I.7A.001 or I.7A.003 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 (CEP) or less.

1.  An ‘integrated navigation system’ typically incorporates the following components:

a.  An inertial measurement device (e.g., an attitude and heading reference system, inertial reference unit, or inertial navigation system);

b.  One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g., satellite navigation receiver, radar altimeter, and/or Doppler radar); and

c.  Integration hardware and software;

2.  In I.7A.004.c. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.7A.005

7A104

Gyro-astro compasses and other devices, which derive position or orientation by means of automatically tracking celestial bodies or satellites and specially designed components therefor.

I.7A.006

7A105

Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS, or Galileo), having any of the following characteristics, and specially designed components therefor:

a.  Designed or modified for use in space launch vehicles specified in I.9A.001, unmanned aerial vehicles specified in I.9A.003 or sounding rockets specified in I.9A.005; or

N.B.: See also Military Goods Controls for receiving equipment for rockets or missiles.

b.  Designed or modified for airborne applications and having any of the following:

1.  Capable of providing navigation information at speeds in excess of 600 m/s;

2.  Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secured signal/data; or

3.  Being specially designed to employ anti-jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures.

Note: I.7A.006.b.2. and I.7A.006.b.3. do not prohibit equipment designed for commercial, civil or ‘Safety of Life’ (e.g., data integrity, flight safety) GNSS services

I.7A.007

7A106

Altimeters of radar or laser radar type, designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

N.B.: See also Military Goods Controls for altimeters for rockets or missiles.

I.7A.008

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 I.9A.001 or sounding rockets specified in I.9A.005.

N.B.: See also Military Goods Controls for passive sensors for rockets or missiles.

Note: I.7A.008 includes sensors for the following equipment:

a.  Terrain contour mapping equipment;

b.  Imaging sensor equipment (both active and passive);

c.  Passive interferometer equipment.

I.7A.009

7A116

Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

N.B.: See also Military Goods Controls for flight control systems and servo valves for rockets or missiles.

a.  Hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems (including fly-by-wire types);

b.  Attitude control equipment;

c.  Flight control servo valves designed or modified for the systems specified in I.7A.009.a. or I.7A.009.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.

I.7A.010

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).

I.7A.011

7B001

Test, calibration or alignment equipment specially designed for equipment specified in I.7A.001 to I.7A.010.

I.7A.012

7B002

Equipment, as follows, specially designed to characterize mirrors for ring ‘laser’ gyros:

N.B.: See also I.7A.014.

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).

I.7A.013

7B003*

Equipment specially designed for the ‘production’ of equipment specified in I.7A.001 to I.7A.010.

Note: I.7A.013 includes:

a.  Gyro tuning test stations;

b.  Gyro dynamic balance stations;

c.  Gyro run-in/motor test stations;

d.  Gyro evacuation and fill stations;

e.  Centrifuge fixtures for gyro bearings;

f.  Accelerometer axis align stations;

g.  (reserved)

h.  Accelerometer test stations;

i.  Inertial measurement unit (IMU) module testers;

j.  Inertial measurement unit (IMU) platform testers;

k.  Inertial measurement unit (IMU) stable element handling fixtures;

l.  Inertial measurement unit (IMU) platform balance fixture.

I.7A.014

7B102

Reflectometers specially designed to characterise mirrors, for ‘laser’ gyros, having a measurement accuracy of 50 ppm or less (better).

I.7A.015

7B103

‘Production facilities’ and ‘production equipment’ as follows:

a.  ‘Production facilities’ specially designed for equipment specified in I.7A.010;

b.  ‘Production equipment’, and other test, calibration and alignment equipment, other than that specified in I.7A.011 to I.7A.013, designed or modified to be used with equipment specified in I.7A.001 to I.7A.010.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.7B.001

ex 7D101

‘Software’ specially designed or modified for the ‘use’ of equipment specified in I.7A.001 to I.7A.008, I.7A.009.a., I.7A.009.b. or I.7A.011 to I.7A.015

I.7B.002

7D102

Integration ‘software’ as follows:

a.  Integration ‘software’ for the equipment specified in I.7A.004.b.;

b.  Integration ‘software’ specially designed for the equipment specified in I.7A.004.a.;

c.  Integration ‘software’ designed or modified for the equipment specified in I.7A.004.c.

Note: A common form of integration ‘software’ employs Kalman filtering.

I.7B.003

7D103

‘Software’ specially designed for modelling or simulation of the ‘guidance sets’ specified in I.7A.010 or for their design integration with the space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

Note:‘Software’ specified in I.7B.003 remains prohibited when combined with specially designed hardware specified in I.4A.003.

I.7B.004

ex 7E001

‘Technology’ according to the General Technology Note for the ‘development’ of equipment or ‘software’ specified in I.7A.001 to I.7A.015, or in I.7B.001 to I.7B.003.

I.7B.005

ex 7E002

‘Technology’ according to the General Technology Note for the ‘production’ of equipment specified in I.7A.001 to I.7A.015.

I.7B.006

7E101

‘Technology’ according to the General Technology Note for the ‘use’ of equipment specified in I.7A.001 to I.7A.015 or I.7B.001 to I.7B.003.

I.7B.007

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 I.7B.007.a. and I.7B.007.b.

I.7B.008

7E104

‘Technology’ for the integration of the flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.9A.001

ex 9A004

Space launch vehicles

N.B.: See also I.9A.005. For rockets and missiles see Military Goods Controls.

Note: I.9A.001 does not prohibit payloads.

I.9A.002

9A011

Ramjet, scramjet or combined cycle engines and specially designed components therefor.

N.B.: See also I.9A.012 and I.9A.016.

I.9A.003

ex 9A012.a

‘Unmanned aerial vehicles’ (‘UAVs’), associated systems, equipment and components as follows:

a.*  ‘UAVs’ having any of the following:

1.*  Having all of the following:

a.  Having any of the following:

1.  An autonomous flight control and navigation capability (e.g., an autopilot with an Inertial Navigation System); or

2.  Capability of controlled-flight out of the direct vision range involving a human operator (e.g., televisual remote control); and

b.  Having any of the following:

1.  Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or

2.  Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or

2.  Capable of delivering a payload to a range of at least 300 km.

1.  An aerosol consists of particulate or liquids other than fuel components, by-products or additives, as part of the payload to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding.

2.  An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream

I.9A.004

9A101

Turbojet and turbofan engines (including turbocompound engines), as follows:

a.  Engines having both of the following characteristics:

1.  Maximum thrust value greater than 400 N (achieved un-installed) excluding civil certified engines with a maximum thrust value greater than 8 890 N (achieved un-installed), and

2.  Specific fuel consumption of 0,15 kg/N/hr or less (at maximum continuous power at sea level static and standard conditions);

b.  Engines designed or modified for use in ‘missiles’.

I.9A.005

9A104

Sounding rockets, capable of a range of at least 300 km.

N.B.: See also I.9A.001. For rockets and missiles see Military Goods Controls.

I.9A.006

9A105

Liquid propellant rocket engines, as follows:

N.B.: See also I.9A.017.

a.  Liquid propellant rocket engines usable in ‘missiles’, having a total impulse capacity equal to or greater than 1,1 MNs;

b.  Liquid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in I.9A.006.a., having a total impulse capacity equal to or greater than 0,841 MNs.

I.9A.007

9A106

Systems or components, usable in ‘missiles’, as follows, specially designed for liquid rocket propulsion systems:

a.  Ablative liners for thrust or combustion chambers;

b.  Rocket nozzles;

c.  Thrust vector control sub-systems;

Technical Note:

Examples of methods of achieving thrust vector control specified in I.9A.007.c. are:

1.  Flexible nozzle;

2.  Fluid or secondary gas injection;

3.  Movable engine or nozzle;

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

5.  Thrust tabs.

d.  Liquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz.

Note: The only servo valves and pumps specified in I.9A.007.d., are the following:

a.  Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms;

b.  Pumps, for liquid propellants, with shaft speeds equal to or greater than 8 000 r.p.m. or with discharge pressures equal to or greater than 7 MPa.

I.9A.008

9A107 and ex 9A007.a

Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, having total impulse capacity equal to or greater than 0,841 MNs.

N.B.: See also I.9A.017.

I.9A.009

9A108

Components usable in ‘missiles’, as follows, specially designed for solid rocket propulsion systems:

a.  Rocket motor cases and ‘insulation’ components therefor;

b.  Rocket nozzles;

c.  Thrust vector control sub-systems.

Technical Note:

Examples of methods of achieving thrust vector control specified in I.9A.009.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.

I.9A.010

9A109

Hybrid rocket motors, usable in ‘missiles’, and specially designed components therefor.

N.B.: See also I.9A.017.

Technical Note:

In I.9A.010 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.9A.011

9A110

Composite structures, laminates and manufactures thereof, specially designed for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005 or the subsystems specified in I.9A.006.a., I.9A.007 to I.9A.009, I.9A.014 or I.9A.017.

N.B.: See also Military Goods Controls for composite structures, laminates and manufactures thereof, for rockets and missiles.

I.9A.012

ex 9A111*

Pulse jet engines, usable in ‘missiles’, and specially designed components therefor.

N.B.: See also I.9A.002 and I.9A.016.

I.9A.013

9A115

Launch support equipment as follows:

N.B.: See also Military Goods Controls for launch support equipment for rockets and missiles.

a.  Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in I.9A.001, unmanned aerial vehicles specified in I.9A.003 or sounding rockets specified in I.9A.005;

b.  Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

I.9A.014

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.

I.9A.015

9A117

Staging mechanisms, separation mechanisms, and interstages, usable in ‘missiles’.

I.9A.016

ex 9A118*

Devices to regulate combustion usable in engines, which are usable in ‘missiles’, specified in I.9A.002 or I.9A.012.

I.9A.017

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 I.9A.006, I.9A.008 and I.9A.010.

I.9A.018

9A120

Liquid propellant tanks specially designed for propellants specified in I.1A.029 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 I.9A.018 ‘other liquid propellants’ includes, but is not limited to, propellants specified in the Military Goods Controls

I.9A.019

(reserved)

I.9A.020

ex 9B105*

Wind tunnels for speeds of Mach 0,9 or more, usable for ‘missiles’ and their subsystems.

I.9A.021

9B106

Environmental chambers and anechoic chambers, as follows:

a.  Environmental chambers capable of simulating the following flight conditions:

1.  Vibration environments equal to or greater than 10 g rms, measured ‘bare table’, between 20 Hz and 2 kHz imparting forces equal to or greater than 5 kN; and

2.  Altitude equal to or greater than 15 km; or

3.  Temperature range of at least 223 K (– 50 °C) to 398 K (+ 125 °C);

1.  I.9A.021.a. describes systems that are capable of generating a vibration environment with a single wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum);

2.  In I.9A.021.a.1. ‘bare table’ means a flat table, or surface with no fixture or fittings.y

b.  Environmental chambers capable of simulating the following flight conditions:

1.  Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 μPa) or with a total rated acoustic power output of 4 kW or greater; and

2.  Altitude equal to or greater than 15 km; or

3.  Temperature range of at least 223 K (– 50 °C) to 398 K (+ 125 °C).

I.9A.022

ex 9B115

Specially designed ‘production equipment’ for the systems, sub-systems and components specified in I.9A.002, I.9A.004, I.9A.006 to I.9A.010, I.9A.012, I.9A.014 to I.9A.017.

I.9A.023

ex 9B116

Specially designed ‘production facilities’ for the space launch vehicles specified in I.9A.001, or systems, sub-systems, and components specified in I.9A.002, I.9A.004, I.9A.005 to I.9A.010, I.9A.012, or I.9A.014 to I.9A.017.

N.B.: See also Military Goods Controls for ‘production facilities’ for rockets and missiles.

I.9A.024

ex 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 90 kN of thrust; or

b.  Capable of simultaneously measuring the three axial thrust components.

I.9A.025

9C108

‘Insulation’ material in bulk form and ‘interior lining’, for rocket motor cases usable in ‘missiles’ or specially designed for ‘missiles’.

Technical Note:

In I.9A.025‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.

I.9A.026

9C110

Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in I.9A.011, 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 I.1A.024 and I.1A.034.

Note: The only resin impregnated fibre prepregs specified in entry I.9A.026 are those using resins with a glass transition temperature (Tg), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.

No

Relevant item(s) from Annex to Regulation (EC) No 1183/2007

Description

I.9B.001

ex 9D001

‘Software’ specially designed or modified for the ‘development’ of equipment or ‘technology’ specified in I.9A.002, I.9A.009, I.9A.012, I.9A.015 or I.9A.016.

I.9B.002

9D101

‘Software’ specially designed or modified for the ‘use’ of goods specified in I.9A.020, I.9A.021, I.9A.023 or I.9A.024.

I.9B.003

9D103

‘Software’ specially designed for modelling, simulation or design integration of the space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005, or the subsystems specified in I.9A.006.a., I.9A.007, I.9A.009, I.9A.014 or I.9A.017.

Note:‘Software’ specified in I.9B.003 remains prohibited when combined with specially designed hardware specified in I.4A.003.

I.9B.004

ex 9D104

‘Software’ specially designed or modified for the ‘use’ of ►C1  goods specified in I.9A.002 ◄ , I.9A.004, I.9A.006, I.9A.007.c., I.9A.007.d., I.9A.008, I.9A.009.c., I.9A.010, I.9A.012, I.9A.013.a., I.9A.014.d., I.9A.015 or I.9A.016.

I.9B.005

9D105

‘Software’ which coordinates the function of more than one subsystem, specially designed or modified for ‘use’ in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.

I.9B.006

ex 9E001

‘Technology’ according to the General Technology Note for the ‘development’ of equipment or ‘software’ specified in I.9A.001, I.9A.003, I.9A.021 to I.9A.024, or I.9B.002 to I.9B.005.

I.9B.007

ex 9E002

‘Technology’ according to the General Technology Note for the ‘production’ of equipment specified in I.9A.001, I.9A.003 or I.9A.021 to I.9A.024.

I.9B.008

9E101

‘Technology’ according to the General Technology Note for the ‘development’ or ‘production’ of goods specified in I.9A.004 to I.9A.017.

I.9B.009

ex 9E102

‘Technology’ according to the General Technology Note for the ‘use’ of space launch vehicles specified in I.9A.001, or goods specified in I.9A.002, I.9A.004 to I.9A.017, I.9A.020 to I.9A.024, I.9B.002 or I.9B.003.

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

IA.A0.001

Hollow cathode lamps as follows:

a.  Iodine hollow cathode lamps with windows in pure silicon or quartz

b.  Uranium hollow cathode lamps

–

IA.A0.005

Nuclear reactor vessel components and testing equipment, other than those specified in 0A001, as follows:

1.  Seals

2.  Internal components

3.  Sealing, testing and measurement equipment

0A001

IA.A0.006

Nuclear detection systems for detection, identification or quantification of radioactive materials and radiation of nuclear origin and specially designed components thereof other than those specified in 0A001.j. or 1A004.c.

0A001.j

1A004.c

IA.A0.007

Bellows-sealed valves made of aluminium alloy or stainless steel type 304, 304L or 316L.

Note: This item does not cover bellow valves defined in 0B001.c.6 and 2A226.

0B001.c.6

2A226

IA.A0.012

Shielded enclosures for the manipulation, storage and handling of radioactive substances (Hot cells).

0B006

IA.A0.013

‘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, other than those specified in 0C001.

0C001

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

IA.A1.001

Bis(2-ethylhexyl) phosphoric acid (HDEHP or D2HPA) CAS 298-07-7 solvent in any quantity, with a purity greater than 90 %.

–

IA.A1.002

Fluorine gas (Chemical Abstract Number (CAS): 7782-41-4), with a purity of at least 95 %.

–

IA.A1.005

Electrolytic cells for fluorine production with an output capacity greater than 100 g of fluorine per hour.

Note: This item does not cover electrolytic cells defined in item 1B225.

1B225

IA.A1.008

Magnetic metals, of all types and of whatever form, having an initial relative permeability of 120 000 or more and a thickness between 0,05 and 0,1 mm.

1C003.a

IA.A1.009

‘Fibrous or filamentary materials’ or prepregs, as follows:

a.  Carbon or aramid ‘fibrous or filamentary materials’ having either of the following characteristics:

1.  A ‘specific modulus’ exceeding 10 × 106 m; or

2.  A ‘specific tensile strength’ exceeding 17 × 104 m;

b.  Glass ‘fibrous or filamentary materials’ having either of the following characteristics:

1.  A ‘specific modulus’ exceeding 3,18 × 106 m; or

2.  A ‘specific tensile strength’ exceeding 76,2 × 103 m;

c.  Thermoset resin-impregnated continuous ‘yarns’, ‘rovings’, ‘tows’ or ‘tapes’ with a width of 15 mm or less (once prepregs), made from carbon or glass ‘fibrous or filamentary materials’ other than those specified in II.A1.010.a. or b.

Note: This item does not cover fibrous or filamentary materials defined in items 1C010.a, 1C010.b, 1C210.a and 1C210.b.

1C010.a

1C010.b

1C210.a

1C210.b

IA.A1.010

Resin-impregnated or pitch-impregnated fibres (prepregs), metal or carbon-coated fibres (preforms) or ‘carbon fibre preforms’, as follows:

a.  Made from ‘fibrous or filamentary materials’ specified in II.A1.009 above;

b.  Epoxy resin ‘matrix’ impregnated carbon ‘fibrous or filamentary materials’ (prepregs), specified in 1C010.a, 1C010.b or 1C010.c, for the repair of aircraft structures or laminates, of which the size of individual sheets does not exceed 50 cm × 90 cm;

c.  Prepregs specified in 1C010.a, 1C010.b or 1C010.c, when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160 °C) and a cure temperature lower than the glass transition temperature.

Note: This item does not cover fibrous or filamentary materials defined in item 1C010.e.

1C010.e.

1C210

IA.A1.011

Reinforced silicon carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in ‘missiles’, other than those specified in 1C107.

1C107

IA.A1.012

Maraging steels, other than those specified in 1C116 or 1C216, ‘capable of’ an ultimate tensile strength of 2 050 MPa or more, at 293 K (20 °C).

Technical note: The phrase ‘maraging steel capable of’ encompasses maraging steel before or after heat treatment.

1C216

IA.A1.013

Tungsten, tantalum, tungsten carbide, tantalum carbide and alloys, having both of the following characteristics:

a.  In forms having a hollow cylindrical or spherical symmetry (including cylinder segments) with an inside diameter between 50 mm and 300 mm; and

b.  A mass greater than 5 kg.

Note: This item does not cover tungsten, tungsten carbide and alloys defined in item 1C226.

1C226

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

IA.A2.001

Vibration test systems, equipment and components thereof, other than those specified in 2B116:

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 0,1g rms between 0,1 Hz and 2 kHz and 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 bandwidth greater than 5 kHz designed for use with vibration test systems specified in a.;

c.  Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured ‘bare table’, and usable in vibration test systems specified in 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 a.

Technical note: ‘Bare table’ means a flat table, or surface, with no fixture or fittings.

2B116

IA.A2.004

Remote manipulators that can be used to provide remote actions in radiochemical separation operations or hot cells, other than those specified in 2B225, having either of the following characteristics:

a.  A capability of penetrating a hot cell wall of 0,3 m or more (through the wall operation); or

b.  A capability of bridging over the top of a hot cell wall with a thickness of 0,3 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.

2B225

IA.A2.011

Centrifugal separators, capable of continuous separation without the propagation of aerosols and manufactured from:

1.  Alloys with more than 25 % nickel and 20 % chromium by weight;

2.  Fluoropolymers;

3.  Glass (including vitrified or enamelled coating or glass lining);

4.  Nickel or alloys with more than 40 % nickel by weight;

5.  Tantalum or tantalum alloys;

6.  Titanium or titanium alloys; or

7.  Zirconium or zirconium alloys.

Note: This item does not cover centrifugal separators defined in item 2B352.c.

2B352.c

IA.A2.012

Sintered metal filters made of nickel or nickel alloy with more than 40 % nickel by weight.

Note: This item does not cover filters defined in item 2B352.d.

2B352.d

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

IA.A3.001

High voltage direct current power supplies having both of the following characteristics:

a.  Capable of continuously producing, over a time period of eight hours, 10 kV or more, with output power of 5 kW or more with or without sweeping; and

b.  Current or voltage stability better than 0,1 % over a time period of four hours.

Note: This item does not cover power supplies defined in items 0B001.j.5 and 3A227.

3A227

IA.A3.002

Mass spectrometers, other than those specified in 3A233 or 0B002.g, capable of measuring ions of 200 atomic mass units or more and having a resolution of better than 2 parts in 200, as follows, and ion sources thereof:

a.  Inductively coupled plasma mass spectrometers (ICP/MS);

b.  Glow discharge mass spectrometers (GDMS);

c.  Thermal ionisation mass spectrometers (TIMS);

d.  Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with ‘materials resistant to corrosion by uranium hexafluoride UF6’;

e.  Molecular beam mass spectrometers having either of the following characteristics:

1.  A source chamber constructed from, lined with or plated with stainless steel or molybdenum and equipped with a cold trap capable of cooling to 193 K (– 80°C) or less; or

2.  A source chamber constructed from, lined with or plated with ‘materials resistant to corrosion by uranium hexafluoride (UF6)’;

f.  Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides.

3A233

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

IA.A6.001

Yttrium aluminium garnet (YAG) rods

–

IA.A6.003

Wave front corrector systems for use with a laser beam having a diameter exceeding 4 mm, and specially designed components thereof, including control systems, phase front sensors and ‘deformable mirrors’ including bimorph mirrors.

Note: This item does not cover mirrors defined in 6A004.a, 6A005.e and 6A005.f.

6A003

IA.A6.004

Argon ion ‘lasers’ having an average output power equal to or greater than 5 W.

Note: This item does not cover argon ion ‘lasers’ defined in items 0B001.g.5, 6A005 and 6A205.a.

6A005.a.6

6A205.a

IA.A6.006

Tunable semiconductor ‘lasers’ and tunable semiconductor ‘laser’ arrays, of a wavelength between 9 μm and 17 μm, as well as array stacks of semiconductor ‘lasers’ containing at least one tunable semiconductor ‘laser’ array of such wavelength.

1.  Semiconductor ‘lasers’ are commonly called ‘laser’ diodes.

2.  This item does not cover semiconductor ‘lasers’ defined in items 0B001.h.6 and 6A005.b

6A005.b

IA.A6.008

Neodymium-doped (other than glass) ‘lasers’, having an output wavelength greater than 1 000 nm but not exceeding 1 100 nm and output energy exceeding 10 J per pulse.

Note: This item does not cover neodymium-doped (other than glass) ‘lasers’ defined in item 6A005.c.2.b.

6A005.c.2

IA.A6.010

Radiation-hardened cameras, or lenses thereof, other than those specified in 6A203.c., 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.

6A203.c

IA.A6.011

Tunable pulsed dye laser amplifiers and oscillators, having all of the following characteristics:

1.  Operating at wavelengths between 300 nm and 800 nm;

2.  An average output power greater than 10 W but not exceeding 30 W;

3.  A repetition rate greater than 1 kHz; and

4.  Pulse width less than 100 ns.

1.  This item does not cover single mode oscillators.

2.  This item does not cover tunable pulsed dye laser amplifiers and oscillators defined in item 6A205.c, 0B001.g.5 and 6A005.

6A205.c

IA.A6.012

Pulsed carbon dioxide ‘lasers’ having all of the following characteristics:

1.  Operating at wavelengths between 9 000 nm and 11 000 nm;

2.  A repetition rate greater than 250 Hz;

3.  An average output power greater than 100 W but not exceeding 500 W; and

4.  Pulse width less than 200 ns.

Note: This item does not cover pulsed carbon dioxide laser amplifiers and oscillators defined in item 6A205.d., 0B001.h.6. and 6A005.d.

6A205.d

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

IA.B.001

Technology required for the development, production, or use of the items in Part IA.A. (Goods) above.

–

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

II.A0.002

Faraday isolators in the wavelength range 500 nm – 650 nm

–

II.A0.003

Optical gratings in the wavelength range 500 nm – 650 nm

–

II.A0.004

Optical fibres in the wavelength range 500 nm – 650 nm coated with anti-reflecting layers in the wavelength range 500 nm – 650 nm and having a core diameter greater than 0,4 mm but not exceeding 2 mm

–

II.A0.008

Plane, convex and concave mirrors, coated with high reflecting or controlled multi-layers in the wavelength range 500 nm – 650 nm

0B001.g.5

II.A0.009

Lenses, polarisers, half-wave retarder plates (λ/2 plates), quarter-wave retarder plates (λ/4 plates), laser windows in silicon or quartz and rotators, coated with anti-reflecting layers in the wavelength range 500 nm – 650 nm

0B001.g

II.A0.010

Pipes, piping, flanges, fittings made of, or lined with nickel, or nickel alloy containing more than 40 % nickel by weight, other than those specified in 2B350.h.1.

2B350

II.A0.011

Vacuum pumps other than those specified in 0B002.f.2. or 2B231, as follows:

— Turbomolecular pumps having a flowrate equal to or greater than 400 l/s,

— Roots type vacuum roughing pumps having a volumetric aspiration flowrate greater than 200 m3/h.

Bellows-sealed, scroll, dry compressor, and bellows-sealed, scroll, dry vacuum pumps.

0B002.f.2

2B231

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

II.A1.003

Seals and gaskets made of any of the following materials

a.  Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching;

b.  Fluorinated polyimides containing 10 % by weight or more of combined fluorine;

c.  Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine;

d.  Polychlorotrifluoroethylene (PCTFE, e.g. Kel-F ®);

e.  Viton fluoro-elastomers;

f.  Polytetrafluoroethylene (PTFE).

II.A1.004

Personal equipment for detecting radiation of nuclear origin, including personal dosimeters

Note: This item does not cover nuclear detection systems defined in item 1A004.c.

1A004.c

II.A1.006

Platinised catalysts, other than those specified in 1A225, 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 and substitutes thereof.

1B231, 1A225

II.A1.007

Aluminium and its alloys, other than those specified in 1C002.b.4 or 1C202.a, in crude or semi-fabricated form having either of the following characteristics:

a.  Capable of an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); or

b.  Having a tensile strength of 415 MPa or more at 298 K (25 °C).

1C002.b.4

1C202.a

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

II.A2.002

Machine tools for grinding having positioning accuracies with ‘all compensations available’ equal to or less (better) than 15 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis.

Note: This item does not cover machine tools for grinding defined in items 2B201.b and 2B001.c.

2B201.b

2B001.c

II.A2.002a

Components and numerical controls, specially designed for machine tools specified in 2B001, 2B201, or II.A2.002 above.

II.A2.003

Balancing machines and related equipment as follows:

a.  Balancing machines, designed or modified for dental or other medical equipment, having all the following characteristics:

1.  Not capable of balancing rotors/assemblies having a mass greater than 3 kg;

2.  Capable of balancing rotors/assemblies at speeds greater than 12 500 rpm;

3.  Capable of correcting unbalance in two planes or more; and

4.  Capable of balancing to a residual specific unbalance of 0,2 g × mm per kg of rotor mass;

b.  Indicator heads designed or modified for use with machines specified in a. above.

Technical note: Indicator heads are sometimes known as balancing instrumentation.

2B119

II.A2.005

Controlled atmosphere heat treatment furnaces, as follows:

Furnaces capable of operation at temperatures above 400 °C.

2B226, 2B227

II.A2.006

Oxidation furnaces capable of operation at temperatures above 400 °C

2B226, 2B227

II.A2.007

‘Pressure transducers’, other than those defined in 2B230, capable of measuring absolute pressures at any point in the range 0 to 200 kPa and having both of the following characteristics:

a.  Pressure sensing elements made of or protected by ‘Materials resistant to corrosion by uranium hexafluoride (UF6)’, and

b.  Having either of the following characteristics:

1.  A full scale of less than 200 kPa and an ‘accuracy’ of better than ± 1 % of full scale; or

2.  A full scale of 200 kPa or greater and an ‘accuracy’ of better than 2 kPa.

Technical note: For the purposes of 2B230, ‘accuracy’ includes non-linearity, hysteresis and repeatability at ambient temperature.

2B230

II.A2.008

Liquid-liquid contacting equipment (mixer-settlers, pulsed columns, centrifugal contactors); and liquid distributors, vapour distributors or liquid collectors designed for such equipment, where all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

1.  Alloys with more than 25 % nickel and 20 % chromium by weight;

2.  Fluoropolymers;

3.  Glass (including vitrified or enamelled coating or glass lining);

4.  Graphite or ‘carbon graphite’;

5.  Nickel or alloys with more than 40 % nickel by weight;

6.  Tantalum or tantalum alloys;

7.  Titanium or titanium alloys;

8.  Zirconium or zirconium alloys; or

9.  Stainless steel.

Technical note: ‘Carbon graphite’ is a composition consisting of amorphous carbon and graphite, in which the graphite content is 8 % or more by weight.

2B350.e

II.A2.009

Industrial equipment and components, other than those specified in 2B350.d, as follows:

Heat exchangers or condensers with a heat transfer surface area greater than 0,05 m2, and less than 30 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 fluid(s) are made from any of the following materials:

1.  Alloys with more than 25 % nickel and 20 % chromium by weight;

2.  Fluoropolymers;

3.  glass (including vitrified or enamelled coating or glass lining);

4.  Graphite or ‘carbon graphite’;

5.  Nickel or alloys with more than 40 % nickel by weight;

6.  Tantalum or tantalum alloys;

7.  Titanium or titanium alloys;

8.  Zirconium or zirconium alloys;

9.  Silicon carbide;

10.  Titanium carbide; or

11.  Stainless steel.

Note: This item does not cover vehicle radiators.

2B350.d

II.A2.010

Multiple-seal, and seal-less pumps, other than those specified in 2B350.i, suitable for corrosive fluids, 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 [measured under standard temperature (273 K or 0 °C) and pressure (101,3 kPa) conditions]; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from any of the following materials:

1.  Stainless steel,

2.  Aluminium alloy.

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

II.A6.002

Infrared optics in the wavelength range 9 μm – 17 μm and components thereof, including cadmium telluride (CdTe) components.

Note: This item does not cover cameras and components defined in item 6A003.

6A003

II.A6.005

Semiconductor ‘lasers’ and components thereof, as follows:

a.  Individual semiconductor ‘lasers’ with an output power greater than 200 mW each, in quantities larger than 100;

b.  Semiconductor ‘laser’ arrays having an output power greater than 20 W.

1.  Semiconductor ‘lasers’ are commonly called ‘laser’ diodes.

2.  This item does not cover ‘lasers’ defined in items 0B001.g.5, 0B001.h.6 and 6A005.b.

3.  This item does not cover ‘laser’ diodes with a wavelength in the range 1 200 nm – 2 000 nm.

6A005.b

II.A6.007

Solid state ‘tunable’‘lasers’ and specially designed components thereof as follows:

a.  Titanium-sapphire lasers,

b.  Alexandrite lasers.

Note: This item does not cover titanium-sapphire and alexandrite lasers defined in items 0B001.g.5, 0B001.h.6 and 6A005.c.1.

6A005.c.1

II.A6.009

Components of acousto-optics, as follows:

a.  Framing tubes and solid-state imaging devices having a recurrence frequency equal to or exceeding 1 kHz;

b.  Recurrence frequency supplies;

c.  Pockels cells.

6A203.b.4.c

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

II.A7.001

Inertial navigation systems and specially designed components thereof, as follows:

I.  Inertial navigation systems which are certified for use on ‘civil aircraft’ by civil authorities of a State participating in the Wassenaar Arrangement, and specially designed components thereof, as follows:

a.  Inertial navigation systems (INS) (gimballed or strapdown) and inertial equipment designed for ‘aircraft’, land vehicle, vessels (surface or underwater) or ‘spacecraft’ for attitude, guidance or control, having any of the following characteristics, and specially designed components thereof:

1.  Navigation error (free inertial) subsequent to normal alignment of 0,8 nautical mile per hour (nm/hr) ‘Circular Error Probable’ (CEP) or less (better); or

2.  specified to function at linear acceleration levels exceeding 10 g;

b.  Hybrid Inertial Navigation Systems embedded with Global Navigation Satellite System(s) (GNSS) or with ‘Data-Based Referenced Navigation’ (‘DBRN’) System(s) for attitude, guidance or control, subsequent to normal alignment, having an INS navigation position accuracy, after loss of GNSS or ‘DBRN’ for a period of up to four minutes, of less (better) than 10 metres ‘Circular Error Probable’ (CEP);

c.  Inertial Equipment for Azimuth, Heading, or North Pointing having any of the following characteristics, and specially designed components thereof:

1.  Designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc / minutes RMS at 45 degrees latitude; or

2.  Designed to have a non-operating shock level of at least 900 g at a duration of at least 1 msec.

Note: The parameters of I.a. and I.b. are applicable with any of the following environmental conditions:

1.  Input random vibration with an overall magnitude of 7,7 g rms in the first half hour and a total test duration of one and a half hours per axis in each of the three perpendicular axes, when the random vibration meets the following:

a.  A constant power spectral density (PSD) value of 0,04 g2/Hz over a frequency interval of 15 to 1 000 Hz; and

b.  The PSD attenuates with a frequency from 0,04 g2/Hz to 0,01 g2/Hz over a frequency interval from 1 000 to 2 000 Hz;

2.  A roll and yaw rate equal to or greater than + 2,62 radian/s (150 deg/s); or

3.  According to national standards equivalent to 1. or 2. above.

1.  I.b. refers to systems in which an INS and other independent navigation aids are built into a single unit (embedded) in order to achieve improved performance.

2.  ‘Circular Error Probable’ (CEP) – In a circular normal distribution, the radius of the circle containing 50 percent of the individual measurements being made, or the radius of the circle within which there is a 50 percent probability of being located.

II.  Theodolite systems incorporating inertial equipment specially designed for civil surveying purposes and designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc minutes RMS at 45 degrees latitude, and specially designed components thereof.

III.  Inertial or other equipment using accelerometers specified in 7A001 or 7A101, where such accelerometers are specially designed and developed as MWD (Measurement While Drilling) sensors for use in downhole well services operations.

7A003, 7A103

No

Description

Related item from Annex I to Regulation (EC) No 1183/2007

II.B.001

Technology required for the development, production or use of the items in Part A. II. (Goods) above.

Name

Identifying information

Reasons

Date of listing

1.

Reza AGHAZADEH

DoB: 15.3.1949 Passport number: S4409483 valid 26.4.2000 – 27.4.2010 Issued: Tehran, Diplomatic passport number: D9001950, issued on 22.1.2008 valid until 21.1.2013, Place of birth: Khoy

Head of the Atomic Energy Organisation of Iran (AEOI). The AEOI oversees Iran’s nuclear programme and is designated under UNSCR 1737 (2006).

24.4.2007

2.

IRGC Brigadier-General Javad DARVISH-VAND

MODAFL Deputy for Inspection. Responsible for all MODAFL facilities and installations

24.6.2008

3.

IRGC Brigadier-General Seyyed Mahdi FARAHI

Managing Director of the Defence Industries Organisation (DIO) which is designated under UNSCR 1737 (2006)

24.6.2008

4.

Dr Hoseyn (Hossein) FAQIHIAN

Address of NFPC: AEOI-NFPD, P.O. Box: 11365-8486, Tehran/Iran

Deputy and Director-General of the Nuclear Fuel Production and Procurement Company (NFPC), part of the AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006). The NFPC involved in enrichment-related activities that Iran is required by the IAEA Board and Security Council to suspend.

24.4.2007

5.

Engineer Mojtaba HAERI

MADAFL Deputy for Industry. Supervisory role over AIO and DIO

24.6.2008

6.

IRGC Brigadier-General Ali HOSEYNITASH

Head of the General Department of the Supreme National Security Council and involved in formulating policy on the nuclear issue

24.6.2008

7.

Mohammad Ali JAFARI, IRGC

Occupe un poste de commandement au sein des IRGC

24.6.2008

8.

Mahmood JANNATIAN

Deputy Head of the Atomic Energy Organisation of Iran

24.6.2008

9.

Said Esmail KHALILIPOUR

DoB: 24.11.1945, PoB: Langroud

Deputy Head of AEOI. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).

24.4.2007

10.

Ali Reza KHANCHI

Address of NRC: AEOI-NRC P.O. Box: 11365-8486 Tehran/Iran; Fax: (+9821) 8021412

Head of AEOI's Tehran Nuclear Research Centre. The IAEA is continuing to seek clarification from Iran about plutonium separation experiments carried out at the TNRC, including about the presence of HEU particles in environmental samples taken at the Karaj Waste Storage Facility where containers used to store depleted uranium targets used in those experiments are located. The AEOI oversees Iran's nuclear programme and is designated under UNSCR 1737 (2006).

24.4.2007

11.

Ebrahim MAHMUDZADEH

Managing Director of Iran Electronic Industries

24.6.2008

12.

Brigadier-General Beik MOHAMMADLU

MODAFL Deputy for Supplies and Logistics

24.6.2008

13.

Anis NACCACHE

Administrateur des Barzagani Tejarat Tavanmad Saccal companies; sa société a tenté d’acquérir des biens sensibles, au bénéfice d’entités listées au titre de la résolution 1737

24.6.2008

14.

Brigadier-General Mohammad NADERI

Head of Aerospace Industries Organisation (AIO), AIO a participé à des programmes sensibles iraniens

24.6.2008

15.

IRGC Brigadier-General Mostafa Mohammad NAJJAR

Minister of MODAFL, responsable de l’ensemble des programmes militaires, y compris des programmes de missiles balistiques.

24.6.2008

16.

Dr Javad RAHIQI

DoB: 21.4.1954, PoB: Mashad

Head of AEOI's Esfahan Nuclear Technology Centre. This oversees the uranium conversion plant at Esfahan. Iran is required by the IAEA Board and the Security Council to suspend all enrichment-related activities. This includes all uranium conversion work. AEOI oversees Iran’s nuclear programme and is designated under UNSCR 1737 (2006).

24.4.2007

17.

Rear Admiral Mohammad SHAFI’I RUDSARI

MODAFL Deputy for Co-ordination

24.6.2008

18.

IRGC Brigadier-General Ali SHAMSHIRI

MODAFL Deputy for Counter-Intelligence, responsible for security of MODAFL personnel and Installations

24.6.2008

19.

Abdollah SOLAT SANA

Managing Director of the Uranium Conversion Facility (UCF) in Esfahan. This is the facility that produces the feed material (UF6) for the enrichment facilities at Natanz. On 27 August 2006, Solat Sana received a special award from President Ahmadinejad for his role.

24.4.2007

20.

IRGC Brigadier-General Ahmad VAHIDI

Deputy Head of MODAFL

24.6.2008

Name

Identifying information

Reasons

Date of listing

1.

Aerospace Industries Organisation, AIO

AIO, 28 Shian 5, Lavizan, Tehran

AIO oversees Iran’s production of missiles, including Shahid Hemmat Industrial Group, Shahid Bagheri Industrial Group and Fajr Industrial Group, which were all designated under UNSCR 1737 (2006). The head of AIO and two other senior officials were also designated under UNSCR 1737 (2006)

24.4.2007

2.

Armament Industries

Pasdaran Av., P.O. Box 19585/777, Tehran

A subsidiary of the DIO (Defence Industries Organisation).

24.4.2007

3.

Armed Forces Geographical Organisation

Assessed to provide geospatial data for the Ballistic Missile programme

24.6.2008

4.

Bank Melli, Melli Bank Iran and all branches and subsidiaries including

Ferdowsi Avenue, P.O. Box 11365-171, Tehran

Providing or attempting to provide financial support for companies which are involved in or procure goods for Iran’s nuclear and missile programmes (AIO, SHIG, SBIG, AEOI, Novin Energy Company, Mesbah Energy Company, Kalaye Electric Company and DIO). Bank Melli serves as a facilitator for Iran’s sensitive activities. It has facilitated numerous purchases of sensitive materials for Iran’s nuclear and missile programmes. It has provided a range of financial services on behalf of entities linked to Iran's nuclear and missile industries, including opening letters of credit and maintaining accounts. Many of the above companies have been designated by UNSCRs 1737 and 1747.

24.6.2008

(a)  Melli Bank plc

London Wall, 11th floor, London EC2Y 5EA, United Kingdom

(b)  Bank Melli Iran Zao

Number 9/1, Ulitsa Mashkova, Moscow, 130064, Russia

5.

Defence Technology and Science Research Centre (DTSRC) – also known as the Educational Research Institute/Moassese Amozeh Va Tahgiaghati (ERI/MAVT Co.)

Pasdaran Av., P.O. Box 19585/777, Tehran

Responsible for R&D. A subsidiary of the DIO. The DTSRC handles much of the procurement for the DIO.

24.4.2007

6.

Iran Electronic Industries

P.O. Box 18575-365, Tehran, Iran

Wholly-owned subsidiary of MODAFL (and therefore a sister-organisation to AIO, AvIO and DIO). Its role is to manufacture electronic components for Iranian weapons systems.

24.6.2008

7.

IRGC Air Force

Operates Iran’s inventory of short and medium range ballistic missiles. The head of the IRGC air force was designated by UNSCR 1737.

24.6.2008

8.

Khatem-ol Anbiya Construction Organisation

Number 221, North Falamak-Zarafshan Intersection, 4th Phase, Shahkrak-E-Ghods, Tehran 14678, Iran

IRGC-owned group of companies. Uses IRGC engineering resources for construction acting as prime contractor on major projects including tunnelling, assessed to support the Iranian ballistic missile and nuclear programmes.

24.6.2008

9.

Malek Ashtar University

Liée au Ministère de la Défense, a crée en 2003 une formation sur les missiles, en étroite collaboration avec l’AIO

24.6.2008

10.

Marine Industries

Pasdaran Av., P.O. Box 19585/777, Tehran

A subsidiary of the DIO.

24.4.2007

11.

Mechanic Industries Group

A participé à la production de composants pour le programme balistique

24.6.2008

12.

Ministry of Defence and Armed Forces Logistics (MODAFL)

West side of Dabestan Street, Abbas Abad District, Tehran

Responsible for Iran’s defence research, development and manufacturing programmes, including support to missile and nuclear programmes

24.6.2008

13.

Ministry of Defence Logistics Export (MODLEX)

P.O. Box 16315-189, Tehran, Iran

It is the export arm of MODAFL, and the agency used for exporting finished weapons in state-to-state transactions. Under UNSCR 1747 (2007) MODLEX should not be trading.

24.6.2008

14.

3M Mizan Machinery Manufacturing

Société écran de l’AIO, participant à des acquisitions dans le domaine balistique.

24.6.2008

15.

Nuclear Fuel Production and Procurement Company (NFPC)

AEOI-NFPD, P.O. Box: 11365-8486, Tehran/Iran

Nuclear Fuel Production Division (NFPD) of AEOI is research and development in the field of nuclear fuel cycle including: uranium exploration, mining, milling, conversion and nuclear waste management. The NFPC is the successor to the NFPD, the subsidiary company under the AEOI that runs research and development in the nuclear fuel cycle including conversion and enrichment

24.4.2007

16.

Parchin Chemical Industries

A travaillé sur des techniques de propulsion pour le programme balistique iranien

24.6.2008

17.

Special Industries Group

Pasdaran Av., P.O. Box 19585/777, Tehran

A subsidiary of the DIO.

24.4.2007

18.

State Purchasing Organisation (SPO)

The SPO appears to facilitate the import of whole weapons. It appears to be a subsidiary of MODAFL

24.6.2008