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CATEGORY 1 - SPECIAL MATERIALS AND RELATED EQUIPMENT

1C Materials

CATEGORY 1 - SPECIAL MATERIALS AND RELATED EQUIPMENT

1C Materials

Technical note:


Metals and alloys:
Unless provision to the contrary is made, the words 'metals' and 'alloys' in 1C001 to 1C012 cover crude and semifabricated forms, as follows:

Crude forms:
Anodes, balls, bars (including notched bars and wire bars), billets, blocks, blooms, brickets, cakes, cathodes, crystals, cubes, dice, grains, granules, ingots, lumps, pellets, pigs, powder, rondelles, shot, slabs, slugs, sponge, sticks;

Semi-fabricated forms (whether or not coated, plated, drilled or punched):
a. Wrought or worked materials fabricated by rolling, drawing, extruding, forging, impact extruding, pressing, graining, atomising, and grinding, i.e.: angles, channels, circles, discs, dust, flakes, foils and leaf, forging, plate, powder, pressings and stampings, ribbons, rings, rods (including bare welding rods, wire rods, and rolled wire), sections, shapes, sheets, strip, pipe and tubes (including tube rounds, squares, and hollows), drawn or extruded wire;
b. Cast material produced by casting in sand, die, metal, plaster or other types of moulds, including high pressure castings, sintered forms, and forms made by powder metallurgy.
The object of the control should not be defeated by the export of non-listed forms alleged to be finished products but representing in reality crude forms or semi-fabricated forms.

1C001 Materials specially designed for use as absorbers of electromagnetic waves, or intrinsically conductive polymers, as follows:

a. Materials for absorbing frequencies exceeding 2 x 10E8 Hz but less than 3 x 10E12 Hz;

b. Materials for absorbing frequencies exceeding 1,5 × 10E14 Hz but less than 37 × 10E14 Hz and not transparent to visible light;

c. Intrinsically conductive polymeric materials with a 'bulk electrical conductivity' exceeding 10000 S/m (Siemens per metre) or a 'sheet (surface) resistivity' of less than 100 ohms/square, based on any of the following polymers:

1. Polyaniline;

2. Polypyrrole;

3. Polythiophene;

4. Poly phenylene-vinylene; or

5. Poly thienylene-vinylene.

1C002 Metal alloys, metal alloy powder and alloyed materials, as follows:

a. Aluminides, as follows:

1. Nickel aluminides containing a minimum of 15 % by weight aluminium, a maximum of 38 % by weight aluminium and at least one additional alloying element;

2. Titanium aluminides containing 10 % by weight or more aluminium and at least one additional alloying element;

b. Metal alloys, as follows, made from the powder or particulate material specified in 1C002.c.:

1. Nickel alloys having any of the following:

a. A 'stress-rupture life' of 10000 hours or longer at 923 K (650 °C) at a stress of 676 MPa; or

b. A 'low cycle fatigue life' of 10000 cycles or more at 823 K (550° C) at a maximum stress of 1095 MPa;

2. Niobium alloys having any of the following:

a. A 'stress-rupture life' of 10000 hours or longer at 1073 K (800 °C) at a stress of 400 MPa; or

b. A 'low cycle fatigue life' of 10000 cycles or more at 973 K (700 °C) at a maximum stress of 700 MPa;

3. Titanium alloys having any of the following:

a. A 'stress-rupture life' of 10000 hours or longer at 723 K (450 °C) at a stress of 200 MPa; or

b. A 'low cycle fatigue life' of 10000 cycles or more at 723 K (450 °C) at a maximum stress of 400 MPa;

4. Aluminium alloys having any of the following:

a. A tensile strength of 240 MPa or more at 473 K (200 °C); or

b. A tensile strength of 415 MPa or more at 298 K (25 °C);

5. Magnesium alloys having all of the following:

a. A tensile strength of 345 MPa or more; and

b. A corrosion rate of less than 1 mm/year in 3 % sodium chloride aqueous solution measured in accordance with ASTM standard G-31 or national equivalents;

c. Metal alloy powder or particulate material, having all of the following:

1. Made from any of the following composition systems:

a. Nickel alloys (Ni-Al-X, Ni-X-Al) qualified for turbine engine parts or components, i.e. with less than 3 non-metallic particles (introduced during the manufacturing process) larger than 100 µm in 10E9 alloy particles;

b. Niobium alloys (Nb-Al-X or Nb-X-Al, Nb-Si-X or Nb-X-Si, Nb-Ti-X or Nb-X-Ti);

c. Titanium alloys (Ti-Al-X or Ti-X-Al);

d. Aluminium alloys (Al-Mg-X or Al-X-Mg, Al-Zn-X or Al-X-Zn, Al-Fe-X or Al-X-Fe); or

e. Magnesium alloys (Mg-Al-X or Mg-X-Al);

2. Made in a controlled environment by any of the following processes:

a. "Vacuum atomisation";

b. "Gas atomisation";

c. "Rotary atomisation";

d. "Splat quenching";

e. "Melt spinning" and "comminution";

f. "Melt extraction" and "comminution"; or

g. "Mechanical alloying"; or

h. "Plasma atomisation"; and

3. Capable of forming materials specified in 1C002.a. or 1C002.b.

d. Alloyed materials having all of the following:

1. Made from any of the composition systems specified in 1C002.c.1.;

2. In the form of uncomminuted flakes, ribbons or thin rods; and

3. Produced in a controlled environment by any of the following:

a. "Splat quenching";

b. "Melt spinning"; or

c. "Melt extraction".

1C003 Magnetic metals, of all types and of whatever form, having any of the following:

a. Initial relative permeability of 120000 or more and a thickness of 0,05 mm or less;

b. Magnetostrictive alloys having any of the following:

1. A saturation magnetostriction of more than 5 × 10E-4; or

2. A magnetomechanical coupling factor (k) of more than 0,8; or

c. Amorphous or 'nanocrystalline' alloy strips, having all of the following:

1. A composition having a minimum of 75 % by weight of iron, cobalt or nickel;

2. A saturation magnetic induction (Bs) of 1,6 T or more; and

3. Any of the following:

a. A strip thickness of 0,02 mm or less; or

b. An electrical resistivity of 2 × 10E-4 ohm cm or more.

1C004 Uranium titanium alloys or tungsten alloys with a "matrix" based on iron, nickel or copper, having all of the following:

a. A density exceeding 17,5 g/cm³;

b. An elastic limit exceeding 880 MPa;

c. An ultimate tensile strength exceeding 1270 MPa; and

d. An elongation exceeding 8 %.

1C005 "Superconductive" "composite" conductors in lengths exceeding 100 m or with a mass exceeding 100 g, as follows:

a. “Superconductive” “composite” conductors containing one or more niobium-titanium ‘filaments’, having both of the following:

1. Embedded in a "matrix" other than a copper or copper-based mixed "matrix"; and

2. Having a cross-section area less than 0,28 × 10E-4 mm² (6 µm in diameter for circular 'filaments');

b. "Superconductive" "composite" conductors consisting of one or more "superconductive" 'filaments' other than niobium-titanium, having all of the following:

1. A "critical temperature" at zero magnetic induction exceeding 9,85 K (-263,31 °C); and

2. Remaining in the "superconductive" state at a temperature of 4,2 K (-268,96 °C) when exposed to a magnetic field oriented in any direction perpendicular to the longitudinal axis of conductor and corresponding to a magnetic induction of 12 T with critical current density exceeding 1750 A/mm² on overall cross-section of the conductor;

c. "Superconductive" "composite" conductors consisting of one or more "superconductive" 'filaments' which remain "superconductive" above 115 K (-158,16 °C).

1C006 Fluids and lubricating materials, as follows:

a. Not used;

2. Chlorofluorocarbons' having all of the following:

a. No 'flash point';

b. An 'autogenous ignition temperature' exceeding 977 K (704 °C);

c. A 'pour point' at 219 K (-54 °C) or less;

d. A 'viscosity index' of 80 or more; and

e. A boiling point at 473 K (200 °C) or higher;

b. Lubricating materials containing, as their principal ingredients, any of the following:

1. Phenylene or alkylphenylene ethers or thio-ethers, or their mixtures, containing more than two ether or thio-ether functions or mixtures thereof; or

2. Fluorinated silicone fluids with a kinematic viscosity of less than 5000 mm²/s (5000 centistokes) measured at 298 K (25 °C);

c. Damping or flotation fluids having all of the following:

1. Purity exceeding 99,8 %;

2. Containing less than 25 particles of 200 μm or larger in size per 100 ml; and

3. Made from at least 85 % of any of the following:

a. Dibromotetrafluoroethane (CAS 25497-30-7, 124-73-2, 27336-23-8);

b. Polychlorotrifluoroethylene (oily and waxy modifications only); or

c. Polybromotrifluoroethylene;

d. Fluorocarbon electronic cooling fluids having all of the following:

1. Containing 85 % by weight or more of any of the following, or mixtures thereof:

a. Monomeric forms of perfluoropolyalkylether-triazines or perfluoroaliphatic-ethers;

b. Perfluoroalkylamines;

c. Perfluorocycloalkanes; or

d. Perfluoroalkanes;

2. Density at 298 K (25 °C) of 1,5 g/ml or more;

3. In a liquid state at 273 K (0 °C); and

4. Containing 60 % or more by weight of fluorine.

1C007 Ceramic powders, non-"composite" ceramic materials, ceramic-"matrix" "composite" materials and precursor materials, as follows

a. Ceramic powders of single or complex borides of titanium, having total metallic impurities, excluding intentional additions, of less than 5 000 ppm, an average particle size equal to or less than 5 µm and no more than 10% of the particles larger than 10 µm

b. Non-"composite" ceramic materials in crude or semi-fabricated form, composed of borides of titanium with a density of 98 % or more of the theoretical density;

c. Ceramic-ceramic "composite" materials with a glass or oxide-"matrix" and reinforced with fibres having all of the following:

1. Made from any of the following materials:

a. Si-N;

b. Si-C;

c. Si-Al-O-N; or

d. Si-O-N; and

2. Having a "specific tensile strength" exceeding 12,7 × 10E3m;

d. Ceramic-ceramic "composite" materials, with or without a continuous metallic phase, incorporating particles, whiskers or fibres, where carbides or nitrides of silicon, zirconium or boron form the "matrix";

e. Precursor materials (i.e., special purpose polymeric or metallo-organic materials) for producing any phase or phases of the materials specified in 1C007.c., as follows:

1. Polydiorganosilanes (for producing silicon carbide);

2. Polysilazanes (for producing silicon nitride);

3. Polycarbosilazanes (for producing ceramics with silicon, carbon and nitrogen components);

f. Ceramic-ceramic "composite" materials with an oxide or glass "matrix" reinforced with continuous fibres from any of the following systems:

1. Al2O3 (CAS 1344-28-1); or

2. Si-C-N.

1C008 Non-fluorinated polymeric substances as follows:

a. Imides, as follows:

1. Bismaleimides;

2. Aromatic polyamide-imides (PAI) having a ‘glass transition temperature (Tg)’ exceeding 563 K (290 °C);

3. Aromatic polyimides having a 'glass transition temperature (Tg)' exceeding 505 K (232°C);

4. Aromatic polyetherimides having a 'glass transition temperature (Tg)' exceeding 563 K (290°C);

b. Not used;

c. Not used;

d. Polyarylene ketones;

e. Polyarylene sulphides, where the arylene group is biphenylene, triphenylene or combinations thereof;

f. Polybiphenylenethersulphone having a 'glass transition temperature (Tg)' exceeding 563 K (290°C).

1C009 Unprocessed fluorinated compounds, as follows:

a. Not used;

b. Fluorinated polyimides containing 10 % by weight or more of combined fluorine;

c. Fluorinated phosphazene elastomers containing 30% by weight or more of combined fluorine.

1C010 “Fibrous or filamentary materials”, as follows:

a. Organic “fibrous or filamentary materials”, having both of the following:

1. "Specific modulus" exceeding 12,7 × 10E6 m; and

2. "Specific tensile strength" exceeding 23,5 × 10E4 m;

b. Carbon “fibrous or filamentary materials”, having both of the following:

1. “Specific modulus” exceeding 14,65 × 10E6 m; and

2. “Specific tensile strength” exceeding 26,82 × 10E4 m;

c. Inorganic "fibrous or filamentary materials", having all of the following:

1. "Specific modulus" exceeding 2,54 × 10E6 m; and

2. Melting, softening, decomposition or sublimation point exceeding 1922 K (1649 °C) in an inert environment;

d. "Fibrous or filamentary materials", having any of the following:

1. Composed of any of the following:

a. Polyetherimides specified in 1C008.a.; or

b. Materials specified in 1C008.d. to 1C008.f.; or

2. Composed of materials specified in 1C010.d.1.a. or 1C010.d.1.b. and "commingled" with other fibres specified in 1C010.a., 1C010.b. or 1C010.c.;

e. Fully or partially resin-impregnated or pitch-impregnated “fibrous or filamentary materials” (prepregs), metal or carbon-coated “fibrous or filamentary materials” (preforms) or “carbon fibre preforms”, having all of the following:

1. Having any of the following:

a. Inorganic “fibrous or filamentary materials” specified in 1C010.c.; or

b. Organic or carbon “fibrous or filamentary materials”, having all of the following:

1. “Specific modulus” exceeding 10,15 × 10E6 m; and

2. “Specific tensile strength” exceeding 17,7 × 10E4 m; and

2. Having any of the following:

a. Resin or pitch specified in 1C008 or 1C009.b.;

b. ‘Dynamic Mechanical Analysis glass transition temperature (DMA T g )’ equal to or exceeding 453 K (180 °C) and having a phenolic resin; or

c. ‘Dynamic Mechanical Analysis glass transition temperature (DMA T g )’ equal to or exceeding 505 K (232 °C) and having a resin or pitch, not specified in 1C008 or 1C009.b., and not being a phenolic resin;

1C011 Metals and compounds, as follows:

a. Metals in particle sizes of less than 60 µm whether spherical, atomised, spheroidal, flaked or ground, manufactured from material consisting of 99 % or more of zirconium, magnesium and alloys thereof;

b. Boron or boron alloys, with a particle size of 60 μm or less, as follows:

1. Boron with a purity of 85 % by weight or more;

2. Boron alloys with a boron content of 85 % by weight or more;

c. Guanidine nitrate (CAS 506-93-4);

d. Nitroguanidine (NQ) (CAS 556-88-7).

1C012 Materials as follows:

a. Plutonium in any form with a plutonium isotopic assay of plutonium-238 of more than 50 % by weight;

b. "Previously separated" neptunium-237 in any form.

1C101 Materials and devices for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures, other than those specified in 1C001, usable in 'missiles', "missile" subsystems or unmanned aerial vehicles specified in 9A012.

1C102 Resaturated pyrolized carbon-carbon materials designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

1C107 Graphite and ceramic materials, other than those specified in 1C007, as follows:

a. Fine grain graphites with a bulk density of 1,72 g/cm³ or greater, measured at 288 K (15 °C), and having a grain size of 100 µm or less, usable for rocket nozzles and re-entry vehicle nose tips, which can be machined to any of the following products:

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;

b. Pyrolytic or fibrous reinforced graphites, usable for rocket nozzles and reentry vehicle nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

c. Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in radomes usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

d. Bulk machinable silicon-carbide reinforced unfired ceramic, usable for nose tips usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

e. Reinforced silicon-carbide ceramic composites, usable for nose tips, reentry vehicles and nozzle flaps usable in "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.

1C111 Propellants and constituent chemicals for propellants, other than those specified in 1C011, as follows:

a. Propulsive substances:

1. Spherical or spheroidal aluminium powder other than that specified in the Military Goods Controls, in particle size 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;

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. Metal powders of zirconium, beryllium or magnesium, or alloys of these metals, if at least 90% of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomized, spheroidal, flaked or ground, consisting 97% by weight or more of any of the following:

1. Zirconium;

2. Beryllium; or

3. Magnesium;

b. Metal powders of either boron or boron alloys with a boron content of 85% or more by weight, if at least 90% of the total particles by particle volume or weight are made up of particles of less than 60 μm (determined by measurement techniques such as using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spheroidal, flaked or ground;

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

a. Dinitrogen trioxide (CAS 10544-73-7);

b. Nitrogen dioxide (CAS 10102-44-0)/dinitrogen tetroxide (CAS 10544-72-6);

c. Dinitrogen pentoxide (CAS 10102-03-1);

d. Mixed Oxides of Nitrogen (MON);

e. SEE MILITARY GOODS CONTROLS FOR Inhibited Red Fuming Nitric Acid (IRFNA);

f. SEE MILITARY GOODS CONTROLS AND 1C238 FOR Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen;

4. Hydrazine derivatives as follows:

a. Trimethylhydrazine (CAS 1741-01-1);

b. Tetramethylhydrazine (CAS 6415-12-9);

c. N,N diallylhydrazine (CAS 5164-11-4);

d. Allylhydrazine (CAS 7422-78-8);

e. Ethylene dihydrazine (CAS 6068-98-0);

f. Monomethylhydrazine dinitrate;

g. Unsymmetrical dimethylhydrazine nitrate;

h. Hydrazinium azide (CAS 14546-44-2);

i. 1,1-Dimethylhydrazinium azide (CAS 227955-52-4) / 1,2-Dimethylhydrazinium azide (CAS 299177-50-7);

j. Hydrazinium dinitrate (CAS 13464-98-7);

k. Diimido oxalic acid dihydrazine (CAS 3457-37-2);

l. 2-hydroxyethylhydrazine nitrate (HEHN);

m. See Military Goods Controls for Hydrazinium perchlorate;

n. Hydrazinium diperchlorate (CAS 13812-39-0);

o. Methylhydrazine nitrate (MHN) (CAS 29674-96-2);

p. 1,1-Diethylhydrazine nitrate (DEHN) / 1,2-Diethylhydrazine nitrate (DEHN) (CAS 363453-17-2);

q. 3,6-dihydrazino tetrazine nitrate (1,4-dihydrazine nitrate) (DHTN);

5. High energy density materials, other than that specified in the Military Goods Controls, usable in ‘missiles’ or unmanned aerial vehicles specified in 9A012 or 9A112.a

a. Mixed fuel that incorporate both solid and liquid fuels, such as boron slurry, having a mass-based energy density of 40 × 10E6 J/kg or greater;

b. Other high energy density fuels and fuel additives (e.g. cubane, ionic solutions, JP-10) having a volume-based energy density of 37,5 × 10E9 J/m³ or greater, measured at 20 °C and one atmosphere (101,325 kPa) pressure;

6. Hydrazine replacement fuels as follows:

a. 2-Dimethylaminoethylazide (DMAZ) (CAS 86147-04-8);

b. Polymeric substances:

1. Carboxy-terminated polybutadiene (including carboxyl-terminated polybutadiene) (CTPB);

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

3. Polybutadiene-acrylic acid (PBAA);

4. Polybutadiene acrylic acid acrylonitrile (PBAN) (CAS 25265-19-4 / CAS 68891-50-9);

5. Polytetrahydrofuran polyethylene glycol (TPEG);

6. Polyglycidyl nitrate (PGN or poly-GLYN) (CAS 27814-48- 8).

c. Other propellant additives and agents:

1. SEE MILITARY GOODS CONTROLS FOR Carboranes, decaboranes, pentaboranes and derivatives thereof;

2. Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8);

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

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

5. Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0);

6. Ferrocene derivatives as follows:

a. See Military Goods Controls for catocene;

b. See Military Goods Controls for Ethyl ferrocene ;

c. See Military Goods Controls for Propyl ferrocene;

d. See Military Goods Controls for n-butyl ferrocene;

e. See Military Goods Controls for Pentyl ferrocene;

f. See Military Goods Controls for Dicyclopentyl ferrocene;

g. See Military Goods Controls for Dicyclohexyl ferrocene;

h. See Military Goods Controls for Diethyl ferrocene

i. See Military Goods Controls for Dipropyl ferrocene;

j. See Military Goods Controls for Dibutyl ferrocene

k. See Military Goods Controls for Dihexyl ferrocene

l. Acetyl ferrocene / 1,1’-diacetyl ferrocene;

m. See Military Goods Controls for ferrocene Carboxylic acids;

n. 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.

7. 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR), other than that specified in the Military Goods Controls.

1C116 Maraging steels, useable in 'missiles', having all of the following:

a. Having an ultimate tensile strength, measured at 293 K (20°C), equal to or greater than:

1. 0,9 Gpa in the solution annealed stage; or

2. 1,5 Gpa in the precipitation hardened stage; and

b. Any of the following forms:

1. Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm;

2. Tubular forms with a wall thickness equal to or less than 50 mm and having an inner diameter equal to or greater than 270 mm.

1C117 Materials for the fabrication of ‘missiles’ components as follows:

a. Tungsten and alloys in particulate form with a tungsten content of 97 % by weight or more and a particle size of 50 × 10E–6 m (50 μm) or less;

b. Molybdenum and alloys in particulate form with a molybdenum content of 97 % by weight or more and a particle size of 50 × 10E–6 m (50 μm) or less;

c. Tungsten materials in solid form having all of the following:

1. Any of the following material compositions:

a. Tungsten and alloys containing 97 % by weight or more of tungsten;

b. Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or

c. Silver infiltrated tungsten containing 80 % by weight or more of tungsten; and

2. Able to be machined to any of the following products:

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

b. 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

c. Blocks having a size of 120 mm by 120 mm by 50 mm or greater.

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.

1C202 Alloys, other than those specified in 1C002.b.3. or .b.4., as follows:

a. Aluminium alloys having both of the following characteristics:

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

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

b. Titanium alloys having both of the following characteristics:

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

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

1C210 Fibrous or filamentary materials' or prepregs, other than those specified in 1C010.a., b. or e., as follows:

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

1. A "specific modulus" of 12,7 × 10E6 m or greater; or

2. A "specific tensile strength" of 23,5 × 10E4 m or greater;

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

1. A "specific modulus" of 3,18 × 10E6 m or greater; and

2. A "specific tensile strength" of 7,62 × 10E4 m or greater;

c. Thermoset resin impregnated continuous "yarns", "rovings", "tows" or "tapes" with a width of 15 mm or less (prepregs), made from carbon or glass "fibrous or filamentary materials" specified in 1C210.a. or b.

1C216 Maraging steel, other than that specified in 1C116, 'capable of' an ultimate tensile strength of 1 950 MPa or more, at 293 K (20oC).

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.

1C226 Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten by weight, other than that specified by 1C117, having both of the following characteristics:

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

b. A mass greater than 20 kg.

1C227 Calcium having both of the following characteristics:

a. Containing less than 1000 parts per million by weight of metallic impurities other than magnesium; and

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

1C228 Magnesium having both of the following characteristics:

a. Containing less than 200 parts per million by weight of metallic impurities other than calcium; and

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

1C229 Bismuth having both of the following characteristics:

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

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

1C230 Beryllium metal, alloys containing more than 50 % beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing, other than that specified in the Military Goods Controls.

1C231 Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium compounds containing more than 60 % hafnium by weight, manufactures thereof, and waste or scrap of any of the foregoing.

1C232 Helium-3 (³He), mixtures containing helium-3, and products or devices containing any of the foregoing.

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.

1C234 Zirconium with a hafnium content of less than 1 part hafnium to 500 parts zirconium by weight, as follows: metal, alloys containing more than 50% zirconium by weight, compounds, manufactures thereof, waste or scrap of any of the foregoing, other than those specified in 0A001.f.

1C235 Tritium, tritium compounds, mixtures containing tritium in which the ratio of tritium to hydrogen atoms exceeds 1 part in 1000, and products or devices containing any of the foregoing.

1C236 Radionuclides' appropriate for making neutron sources based on alpha-n reaction, other than those specified in 0C001 and 1C012.a., in the following forms:

a. Elemental;

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

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

d. Products or devices containing any of the foregoing.

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.

1C238 Chlorine trifluoride (ClF3).

1C239 High explosives, other than those specified in the Military Goods Controls, or substances or mixtures containing more than 2 % by weight thereof, with a crystal density greater than 1,8 g/cm³ and having a detonation velocity greater than 8000 m/s.

1C240 Nickel powder and porous nickel metal, other than those specified in 0C005, as follows:

a. Nickel powder having both of the following characteristics:

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

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

b. Porous nickel metal produced from materials specified in 1C240.a.

1C241 Rhenium, and alloys containing 90% by weight or more rhenium; and alloys of rhenium and tungsten containing 90% by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics:

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

b. A mass greater than 20kg.

1C350 Chemicals, which may be used as precursors for toxic chemical agents, as follows, and "chemical mixtures" containing one or more thereof:

1. Thiodiglycol (111-48-8);

2. Phosphorus oxychloride (10025-87-3);

3. Dimethyl methylphosphonate (756-79-6);

4. SEE MILITARY GOODS CONTROLS FOR Methyl phosphonyl difluoride (676-99-3);

5. Methyl phosphonyl dichloride (676-97-1);

6. Dimethyl phosphite (DMP) (868-85-9);

7. Phosphorus trichloride (7719-12-2);

8. Trimethyl phosphite (TMP) (121-45-9);

9. Thionyl chloride (7719-09-7);

10. 3-Hydroxy-1-methylpiperidine (3554-74-3);

11. N,N-Diisopropyl-(beta)-aminoethyl chloride (96-79-7);

12. N,N-Diisopropyl-(beta)-aminoethane thiol (5842-07-9);

13. 3-Quinuclidinol (1619-34-7);

14. Potassium fluoride (7789-23-3);

15. 2-Chloroethanol (107-07-3);

16. Dimethylamine (124-40-3);

17. Diethyl ethylphosphonate (78-38-6);

18. Diethyl-N,N-dimethylphosphoramidate (2404-03-7);

19. Diethyl phosphite (762-04-9);

20. Dimethylamine hydrochloride (506-59-2);

21. Ethyl phosphinyl dichloride (1498-40-4);

22. Ethyl phosphonyl dichloride (1066-50-8);

23. SEE MILITARY GOODS CONTROLS FOR Ethyl phosphonyl difluoride (753-98-0);

24. Hydrogen fluoride (7664-39-3);

25. Methyl benzilate (76-89-1);

26. Methyl phosphinyl dichloride (676-83-5);

27. N,N-Diisopropyl-(beta)-amino ethanol (96-80-0);

28. Pinacolyl alcohol (464-07-3);

29. SEE MILITARY GOODS CONTROLS for O Ethyl O-2 diisopropylaminoethyl methylphosphonite (QL) (57856 11 8);

30. Triethyl phosphite (122-52-1);

31. Arsenic trichloride (7784-34-1);

32. Benzilic acid (76-93-7);

33. Diethyl methylphosphonite (15715-41-0);

34. Dimethyl ethylphosphonate (6163-75-3);

35. Ethyl phosphinyl difluoride (430-78-4);

36. Methyl phosphinyl difluoride (753-59-3);

37. 3-Quinuclidone (3731-38-2);

38. Phosphorus pentachloride (10026-13-8);

39. Pinacolone (75-97-8);

40. Potassium cyanide (151-50-8);

41. Potassium bifluoride (7789-29-9);

42. Ammonium hydrogen fluoride or ammonium bifluoride (1341-49-7);

43. Sodium fluoride (7681-49-4);

44. Sodium bifluoride (1333-83-1);

45. Sodium cyanide (143-33-9);

46. Triethanolamine (102-71-6);

47. Phosphorus pentasulphide (1314-80-3);

48. Di-isopropylamine (108-18-9);

49. Diethylaminoethanol (100-37-8);

50. Sodium sulphide (1313-82-2);

51. Sulphur monochloride (10025-67-9);

52. Sulphur dichloride (10545-99-0);

53. Triethanolamine hydrochloride (637-39-8);

54. N,N-Diisopropyl-(Beta)-aminoethyl chloride hydrochloride (4261-68-1);

55. Methylphosphonic acid (993-13-5);

56. Diethyl methylphosphonate (683-08-9);

57. N,N-Dimethylaminophosphoryl dichloride (677-43-0);

58. Triisopropyl phosphite (116-17-6);

59. Ethyldiethanolamine (139-87-7)

60. O,O-Diethyl phosphorothioate (2465-65-8);

61. O,O-Diethyl phosphorodithioate (298-06-6);

62. Sodium hexafluorosilicate (16893-85-9);

63. Methylphosphonothioic dichloride (676-98-2).

64. Diethylamine (109-89-7).

1C351 Human and animal pathogens and "toxins", as follows:

a. Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

1. African horse sickness virus;

2. African swine fever virus;

3. Andes virus;

4. Avian influenza virus, which are:

a. Uncharacterised; or

b. Defined in Annex I(2) EC Directive 2005/94/EC (O.J. L.10 14.1.2006 p.16) as having high pathogenicity, as follows:

1. Type A viruses with an IVPI (intravenous pathogenicity index) in 6 week old chickens of greater than 1,2; or

2. Type A viruses of the subtypes H5 or H7 with genome sequences codified for multiple basic amino acids at the cleavage site of the haemagglutinin molecule similar to that observed for other HPAI viruses, indicating that the haemagglutinin molecule can be cleaved by a host ubiquitous protease;

5. Bluetongue virus;

6. Chapare virus;

7. Chikungunya virus;

8. Choclo virus;

9. Crimean-Congo hemorrhagic fever virus;

10. Dengue virus;

11. Dobrava-Belgrade virus;

12. Eastern equine encephalitis virus;

13. Ebolavirus: all members of the Ebolavirus genus;

14. Foot-and-mouth disease virus;

15. Goatpox virus;

16. Guanarito virus;

17. Hantaan virus;

18. Hendra virus (Equine morbillivirus);

19. Suid herpesvirus 1 (Pseudorabies virus (Aujeszky's disease);

20. Classical swine fever virus (Hog cholera virus);

21. Japanese encephalitis virus;

22. Junin virus;

23. Kyasanur Forest disease virus;

24. Laguna Negra virus;

25. Lassa virus;

26. Louping ill virus;

27. Lujo virus;

28. Lumpy skin disease virus;

29. Lymphocytic choriomeningitis virus;

30. Machupo virus;

31. Marburgvirus: all members of the Marburgvirus genus;

32. Monkeypox virus;

33. Murray Valley encephalitis virus;

34. Newcastle disease virus;

35. Nipah virus;

36. Omsk haemorrhagic fever virus;

37. Oropouche virus;

38. Peste-des-petits-ruminants virus;

39. Swine vesicular disease virus;

40. Powassan virus;

41. Rabies virus and all other members of the Lyssavirus genus;

42. Rift Valley fever virus;

43. Rinderpest virus;

44. Rocio virus;

45. Sabia virus;

46. Seoul virus;

47. Sheeppox virus;

48. Sin Nombre virus;

49. St Louis encephalitis virus;

50. Porcine Teschovirus;

51. Tick-borne encephalitis virus (Far Eastern subtype);

52. Variola virus;

53. Venezuelan equine encephalitis virus;

54. Vesicular stomatitis virus;

55. Western equine encephalitis virus;

56. Yellow fever virus;

57. Severe acute respiratory syndrome-related coronavirus (SARS-related coronavirus);

58. Reconstructed 1918 influenza virus;

b. Not used;

c. Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

1. Bacillus anthracis;

2. Brucella abortus;

3. Brucella melitensis;

4. Brucella suis;

5. Burkholderia mallei (Pseudomonas mallei);

6. Burkholderia pseudomallei (Pseudomonas pseudomallei);

7. Chlamydophila psittaci (formally known as Chlamydia psittaci);

8. Clostridium argentinense (formerly known as Clostridium botulinum Type G), botulinum neurotoxin producing strains;

9. Clostridium baratii, botulinum neurotoxin producing strains;

10. Clostridium botulinum;

11. Clostridium butyricum, botulinum neurotoxin producing strains;

12. Clostridium perfringens epsilon toxin producing types;

13. Coxiella burnetii;

14. Francisella tularensis;

15. Mycoplasma capricolum subspecies capripneumoniae (strain F38);

16. Mycoplasma mycoides subspecies mycoides SC (small colony);

17. Rickettsia prowasecki;

18. Salmonella typhi;

19. Shiga toxin producing Escherichia coli (STEC) of serogroups O26, O45, O103, O104, O111, O121, O145, O157, and other shiga toxin producing serogroups;

20. Shigella dysenteriae;

21. Vibrio cholerae;

22. Yersinia pestis;

d. "Toxins", as follows, and "sub-unit of toxins" thereof:

1. Botulinum toxins;

2. Clostridium perfringens alpha, beta 1, beta 2, epsilon and iota toxins;

3. Conotoxin;

4. Ricin;

5. Saxitoxin;

6. Shiga toxin;

7. Staphylococcus aureus enterotoxins, hemolysin alpha toxin, and toxic shock syndrome toxin (formerly known as Staphylococcus enterotoxin F);

8. Tetrodotoxin;

9. Verotoxin and shiga-like ribosome inactivating proteins;

10. Microcystin (Cyanginosin);

11. Aflatoxins;

12. Abrin;

13. Cholera toxin;

14. Diacetoxyscirpenol toxin;

15. T-2 toxin;

16. HT-2 toxin;

17. Modeccin toxin;

18. Volkensin toxin;

19. Viscum Album Lectin 1 (Viscumin);

e. Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

1. Coccidioides immitis;

2. Coccidioides posadasii.

1C352 Not used

1C353 Genetic elements and genetically modified organisms, as follows:

a. Genetically modified organisms or genetic elements that contain nucleic acid sequences associated with pathogenicity of organisms specified in 1C351.a., 1C351.c, 1C351.e. or 1C354;

b. Genetically modified organisms or genetic elements that contain nucleic acid sequences coding for any of the "toxins" specified in 1C351.d. or "sub-units of toxins" thereof.

1C354 Plant pathogens, as follows:

a. Viruses, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material including living material which has been deliberately inoculated or contaminated with such cultures, as follows:

1. Andean potato latent virus (Potato Andean latent tymovirus);

2. Potato spindle tuber viroid;

b. Bacteria, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

1. Xanthomonas albilineans;

2. Xanthomonas axonopodis pv. citri (Xanthomonas campestris pv. citri A) [Xanthomonas campestris pv. citri];

3. Xanthomonas oryzae pv. oryzae (Pseudomonas campestris pv. oryzae);

4. Clavibacter michiganensis subsp. sepedonicus (Corynebacterium michiganensis subsp. sepedonicum or Corynebacterium sepedonicum);

5. Ralstonia solanacearum, race 3, biovar 2;

c. Fungi, whether natural, enhanced or modified, either in the form of "isolated live cultures" or as material which has been deliberately inoculated or contaminated with such cultures, as follows:

1. Colletotrichum kahawae (Colletotrichum coffeanum var. virulans);

2. Cochliobolus miyabeanus (Helminthosporium oryzae);

3. Microcyclus ulei (syn. Dothidella ulei);

4. Puccinia graminis ssp. graminis var. graminis / Puccinia graminis ssp. graminis var. stakmanii (Puccinia graminis [syn. Puccinia graminis f. sp. tritici]);

5. Puccinia striiformis (syn. Puccinia glumarum);

6. Magnaporthe oryzae (Pyricularia oryzae);

7. Peronosclerospora philippinensis (Peronosclerospora sacchari);

8. Sclerophthora rayssiae var. zeae;

9. Synchytrium endobioticium;

10. Tilletia indica;

11. Thecaphora solani.

1C450 Toxic chemicals and toxic chemical precursors, as follows, and "chemical mixtures" containing one or more thereof:

a. Toxic chemicals, as follows:

1. Amiton: O,O-Diethyl S-[2-(diethylamino)ethyl] phosphorothiolate (78-53-5) and corresponding alkylated or protonated salts;

2. PFIB: 1,1,3,3,3-Pentafluoro-2-(trifluoromethyl)-1-propene (382-21-8);

3. SEE MILITARY GOODS CONTROLS FOR BZ: 3-Quinuclidinyl benzilate (6581-06-2);

4. Phosgene: Carbonyl dichloride (75-44-5);

5. Cyanogen chloride (506-77-4);

6. Hydrogen cyanide (74-90-8);

7. Chloropicrin: Trichloronitromethane (76-06-2);

b. Toxic chemical precursors, as follows:

1. Chemicals, other than those specified in the Military Goods Controls or in 1C350, containing a phosphorus atom to which is bonded one methyl, ethyl or propyl (normal or iso) group but not further carbon atoms;

2. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] phosphoramidic dihalides, other than N,N-Dimethylaminophosphoryl dichloride;

3. Dialkyl [methyl, ethyl or propyl (normal or iso)] N,N-dialkyl [methyl, ethyl or propyl (normal or iso)]-phosphoramidates, other than Diethyl-N,N-dimethylphosphoramidate which is specified in 1C350;

4. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethyl-2-chlorides and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethyl chloride or N,N-Diisopropyl-(beta)-aminoethyl chloride hydrochloride which are specified in 1C350;

5. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-ols and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethanol (96-80-0) and N,N-Diethylaminoethanol (100-37-8) which are specified in 1C350;

6. N,N-Dialkyl [methyl, ethyl or propyl (normal or iso)] aminoethane-2-thiols and corresponding protonated salts, other than N,N-Diisopropyl-(beta)-aminoethane thiol which is specified in 1C350;

7. See 1C350 for ethyldiethanolamine (139-87-7);

8. Methyldiethanolamine (105-59-9).

General Notes

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Definition of Terms

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Reasons for Control

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CN Codes

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