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Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUCeramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUPyrolytic or fibrous reinforced graphites usable for rocket nozzles and re-entry vehicle nose tips usable in systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUPyrolytic or fibrous reinforced graphites usable for rocket nozzles and re-entry vehicle nose tips usable in systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUFine grain graphites with a bulk density of at least 1.72 g/cc measured at 15ºC and having a grain size of 100 x 10 -6 m (100 μm) or less, usable for rocket nozzles and re-entry vehicle nose tips, which can 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 x 120 mm x 50 mm or greater.
Authority: GBProhibited Supply To: IRProgram: UK-INUFine grain graphites with a bulk density of at least 1.72 g/cc measured at 15ºC and having a grain size of 100 x 10 -6 m (100 μm) or less, usable for rocket nozzles and re-entry vehicle nose tips, which can 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 x 120 mm x 50 mm or greater.
Authority: GBProhibited Supply To: IRProgram: UK-INUResaturated pyrolised (i.e. carbon-carbon) materials having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUResaturated pyrolised (i.e. carbon-carbon) materials having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUResin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7.62 x 10 4 m and a specific modulus greater than 3.18 x 10 6 m.
Authority: GBProhibited Supply To: IRProgram: UK-INUResin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7.62 x 10 4 m and a specific modulus greater than 3.18 x 10 6 m.
Authority: GBProhibited Supply To: IRProgram: UK-INUEquipment and process controls, other than those specified in 6.B.3. or 6.B.4., designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips.
Authority: GBProhibited Supply To: IRProgram: UK-INUEquipment and process controls, other than those specified in 6.B.3. or 6.B.4., designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips.
Authority: GBProhibited Supply To: IRProgram: UK-INUChemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites.
Authority: GBProhibited Supply To: IRProgram: UK-INUChemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites.
Authority: GBProhibited Supply To: IRProgram: UK-INUIsostatic presses having all of the following characteristics: a. Maximum working pressure equal to or greater than 69 MPa; b. Designed to achieve and maintain a controlled thermal environment of 600 o C or greater; and c. Possessing a chamber cavity with an inside diameter of 254 mm or greater.
Authority: GBProhibited Supply To: IRProgram: UK-INUIsostatic presses having all of the following characteristics: a. Maximum working pressure equal to or greater than 69 MPa; b. Designed to achieve and maintain a controlled thermal environment of 600 o C or greater; and c. Possessing a chamber cavity with an inside diameter of 254 mm or greater.
Authority: GBProhibited Supply To: IRProgram: UK-INUNozzles specially designed for the processes referred to in 6.E.3.
Authority: GBProhibited Supply To: IRProgram: UK-INUNozzles specially designed for the processes referred to in 6.E.3.
Authority: GBProhibited Supply To: IRProgram: UK-INUEquipment for the “production” of structural composites, fibres, prepregs or preforms, usable in the systems specified in 1.A., 19.A.1. or 19.A.2., as follows, and specially designed components, and accessories therefor: a. Filament winding machines or fibre placement machines, of which the motions for positioning, wrapping and winding fibres can be co-ordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and co-ordinating and programming controls; b. Tape-laying machines of which the motions for positioning and laying tape and sheets can be co-ordinated and programmed in two or more axes, designed for the manufacture of composite airframes and missile structures; c. Multi-directional, multi-dimensional weaving machines or interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to manufacture composite structures; d. 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); e. Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.
Authority: GBProhibited Supply To: IRProgram: UK-INUEquipment for the “production” of structural composites, fibres, prepregs or preforms, usable in the systems specified in 1.A., 19.A.1. or 19.A.2., as follows, and specially designed components, and accessories therefor: a. Filament winding machines or fibre placement machines, of which the motions for positioning, wrapping and winding fibres can be co-ordinated and programmed in three or more axes, designed to fabricate composite structures or laminates from fibrous or filamentary materials, and co-ordinating and programming controls; b. Tape-laying machines of which the motions for positioning and laying tape and sheets can be co-ordinated and programmed in two or more axes, designed for the manufacture of composite airframes and missile structures; c. Multi-directional, multi-dimensional weaving machines or interlacing machines, including adapters and modification kits for weaving, interlacing or braiding fibres to manufacture composite structures; d. 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); e. Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies.
Authority: GBProhibited Supply To: IRProgram: UK-INUResaturated pyrolised (i.e. carbon-carbon) components having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUResaturated pyrolised (i.e. carbon-carbon) components having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1.
Authority: GBProhibited Supply To: IRProgram: UK-INUComposite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
Authority: GBProhibited Supply To: IRProgram: UK-INUComposite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of equipment specified in 4.B. for the “production” and handling of materials specified in 4.C.
Authority: GBProhibited Supply To: IRProgram: UK-INU“Software” specially designed or modified for the “use” of equipment specified in 4.B. for the “production” and handling of materials specified in 4.C.
Authority: GBProhibited Supply To: IRProgram: UK-INUOther propellant additives and agents as follows: a. Bonding agents as follows: 1. Tris (1-(2-methyl)aziridinyl) phosphine oxide (MAPO) (CAS 57-39-6); 2. 1,1 ′ ,1 ″ -trimesoyl-tris(2-ethylaziridine) (HX-868, BITA) (CAS 7722-73-8); 3. Tepanol (HX-878), reaction product of tetraethlylenepentamine, acrylonitrile and glycidol (CAS 68412-46-4); 4. Tepan (HX-879), reaction product of tetraethlylenepentamine and acrylonitrile (CAS 68412-45-3); 5. Polyfunctional aziridine amides with isophthalic, trimesic, isocyanuric, or trimethyladipic backbone also having a 2-methyl or 2-ethyl aziridine group; ′ . b. Curing reaction catalysts as follows: Triphenyl bismuth (TPB) (CAS 603-33-8); c. Burning rate modifiers, as follows: 1. Carboranes, decaboranes, pentaboranes and derivatives thereof; 2. Ferrocene derivatives, as follows: a. Catocene (CAS 37206-42-1); b. Ethyl ferrocene (CAS 1273-89-8); c. Propyl ferrocene; d. n-Butyl ferrocene (CAS 31904-29-7); e. Pentyl ferrocene (CAS 1274-00-6); f. Dicyclopentyl ferrocene; g. Dicyclohexyl ferrocene; h. Diethyl ferrocene (CAS 1273-97-8); i. Dipropyl ferrocene; j. Dibutyl ferrocene (CAS 1274-08-4); k. Dihexyl ferrocene (CAS 93894-59-8); l. Acetyl ferrocene (CAS 1271-55-2) / 1,1’-diacetyl ferrocene (CAS 1273- 94-5); m. Ferrocene carboxylic acid (CAS 1271-42-7) / 1,1’-Ferrocenedicarboxylic acid (CAS 1293-87-4); n. Butacene (CAS 125856-62-4); o. Other ferrocene derivatives usable as rocket propellant burning rate modifiers; . d. Esters and plasticisers as follows: 1. Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8); 2. Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1); 3. 1,2,4-butanetriol trinitrate (BTTN) (CAS 6659-60-5); 4. Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0); 5. 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR); 6. Nitratoethylnitramine (NENA) based plasticisers, as follows: a. Methyl-NENA (CAS 17096-47-8); b. Ethyl-NENA (CAS 85068-73-1); c. Butyl-NENA (CAS 82486-82-6); 7. Dinitropropyl based plasticisers, as follows: a. Bis (2,2-dinitropropyl) acetal (BDNPA) (CAS 5108-69-0); b. Bis (2,2-dinitropropyl) formal (BDNPF) (CAS 5917-61-3); e. Stabilisers as follows: 1. 2-Nitrodiphenylamine (CAS 119-75-5); 2. N-methyl-p-nitroaniline (CAS 100-15-2).
Authority: GBProhibited Supply To: IRProgram: UK-INUOther propellant additives and agents as follows: a. Bonding agents as follows: 1. Tris (1-(2-methyl)aziridinyl) phosphine oxide (MAPO) (CAS 57-39-6); 2. 1,1 ′ ,1 ″ -trimesoyl-tris(2-ethylaziridine) (HX-868, BITA) (CAS 7722-73-8); 3. Tepanol (HX-878), reaction product of tetraethlylenepentamine, acrylonitrile and glycidol (CAS 68412-46-4); 4. Tepan (HX-879), reaction product of tetraethlylenepentamine and acrylonitrile (CAS 68412-45-3); 5. Polyfunctional aziridine amides with isophthalic, trimesic, isocyanuric, or trimethyladipic backbone also having a 2-methyl or 2-ethyl aziridine group; ′ . b. Curing reaction catalysts as follows: Triphenyl bismuth (TPB) (CAS 603-33-8); c. Burning rate modifiers, as follows: 1. Carboranes, decaboranes, pentaboranes and derivatives thereof; 2. Ferrocene derivatives, as follows: a. Catocene (CAS 37206-42-1); b. Ethyl ferrocene (CAS 1273-89-8); c. Propyl ferrocene; d. n-Butyl ferrocene (CAS 31904-29-7); e. Pentyl ferrocene (CAS 1274-00-6); f. Dicyclopentyl ferrocene; g. Dicyclohexyl ferrocene; h. Diethyl ferrocene (CAS 1273-97-8); i. Dipropyl ferrocene; j. Dibutyl ferrocene (CAS 1274-08-4); k. Dihexyl ferrocene (CAS 93894-59-8); l. Acetyl ferrocene (CAS 1271-55-2) / 1,1’-diacetyl ferrocene (CAS 1273- 94-5); m. Ferrocene carboxylic acid (CAS 1271-42-7) / 1,1’-Ferrocenedicarboxylic acid (CAS 1293-87-4); n. Butacene (CAS 125856-62-4); o. Other ferrocene derivatives usable as rocket propellant burning rate modifiers; . d. Esters and plasticisers as follows: 1. Triethylene glycol dinitrate (TEGDN) (CAS 111-22-8); 2. Trimethylolethane trinitrate (TMETN) (CAS 3032-55-1); 3. 1,2,4-butanetriol trinitrate (BTTN) (CAS 6659-60-5); 4. Diethylene glycol dinitrate (DEGDN) (CAS 693-21-0); 5. 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR); 6. Nitratoethylnitramine (NENA) based plasticisers, as follows: a. Methyl-NENA (CAS 17096-47-8); b. Ethyl-NENA (CAS 85068-73-1); c. Butyl-NENA (CAS 82486-82-6); 7. Dinitropropyl based plasticisers, as follows: a. Bis (2,2-dinitropropyl) acetal (BDNPA) (CAS 5108-69-0); b. Bis (2,2-dinitropropyl) formal (BDNPF) (CAS 5917-61-3); e. Stabilisers as follows: 1. 2-Nitrodiphenylamine (CAS 119-75-5); 2. N-methyl-p-nitroaniline (CAS 100-15-2).
Authority: GBProhibited Supply To: IRProgram: UK-INUPolymeric substances, as follows: a. Carboxy - terminated polybutadiene (including carboxyl - terminated polybutadiene) (CTPB); b. Hydroxy - terminated polybutadiene (including hydroxyl - terminated polybutadiene) (HTPB); c. Glycidyl azide polymer (GAP); d. Polybutadiene - Acrylic Acid (PBAA); e. Polybutadiene - Acrylic Acid - Acrylonitrile (PBAN) ; f. Polytetrahydrofuran polyethylene glycol (TPEG).
Authority: GBProhibited Supply To: IRProgram: UK-INUPolymeric substances, as follows: a. Carboxy - terminated polybutadiene (including carboxyl - terminated polybutadiene) (CTPB); b. Hydroxy - terminated polybutadiene (including hydroxyl - terminated polybutadiene) (HTPB); c. Glycidyl azide polymer (GAP); d. Polybutadiene - Acrylic Acid (PBAA); e. Polybutadiene - Acrylic Acid - Acrylonitrile (PBAN) ; f. Polytetrahydrofuran polyethylene glycol (TPEG).
Authority: GBProhibited Supply To: IRProgram: UK-INUOxidiser substances as follows: a. Oxidiser substances usable in liquid propellant rocket engines as follows: 1. Dinitrogen trioxide (CAS 10544-73-7); 2. Nitrogen dioxide (CAS 10102-44-0) / dinitrogen tetroxide (CAS 10544-72-6); 3. Dinitrogen pentoxide (CAS 10102-03-1); 4. Mixed Oxides of Nitrogen (MON); 5. Inhibited Red Fuming Nitric Acid (IRFNA) (CAS 8007-58-7); 6. Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen; b. Oxidiser substances usable in solid propellant rocket motors as follows: 1. Ammonium perchlorate (AP) (CAS 7790-98-9); 2. Ammonium dinitramide (ADN) (CAS 140456-78-6); 3. Nitro-amines (cyclotetramethylene - tetranitramine (HMX) (CAS 2691-41-0); cyclotrimethylene - trinitramine (RDX) (CAS 121-82-4); 4. Hydrazinium nitroformate (HNF) (CAS 20773-28-8); 5. 2,4,6,8,10,12-Hexanitrohexaazaisowurtzitane (CL-20) (CAS 135285-90-4).
Authority: GBProhibited Supply To: IRProgram: UK-INUOxidiser substances as follows: a. Oxidiser substances usable in liquid propellant rocket engines as follows: 1. Dinitrogen trioxide (CAS 10544-73-7); 2. Nitrogen dioxide (CAS 10102-44-0) / dinitrogen tetroxide (CAS 10544-72-6); 3. Dinitrogen pentoxide (CAS 10102-03-1); 4. Mixed Oxides of Nitrogen (MON); 5. Inhibited Red Fuming Nitric Acid (IRFNA) (CAS 8007-58-7); 6. Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen; b. Oxidiser substances usable in solid propellant rocket motors as follows: 1. Ammonium perchlorate (AP) (CAS 7790-98-9); 2. Ammonium dinitramide (ADN) (CAS 140456-78-6); 3. Nitro-amines (cyclotetramethylene - tetranitramine (HMX) (CAS 2691-41-0); cyclotrimethylene - trinitramine (RDX) (CAS 121-82-4); 4. Hydrazinium nitroformate (HNF) (CAS 20773-28-8); 5. 2,4,6,8,10,12-Hexanitrohexaazaisowurtzitane (CL-20) (CAS 135285-90-4).
Authority: GBProhibited Supply To: IRProgram: UK-INUOxidisers/Fuels as follows: Perchlorates, chlorates or chromates mixed with powdered metals or other high energy fuel components.
Authority: GBProhibited Supply To: IRProgram: UK-INUOxidisers/Fuels as follows: Perchlorates, chlorates or chromates mixed with powdered metals or other high energy fuel components.
Authority: GBProhibited Supply To: IRProgram: UK-INUFuel substances as follows: a. Hydrazine (CAS 302-01 - 2) with a concentration of more than 70%; b. Hydrazine derivatives as follows: 1. Monomethylhydrazine (MMH) (CAS 60-34 - 4); 2. Unsymmetrical dimethylhydrazine (UDMH) (CAS 57-14-7); 3. Hydrazine mononitrate; 4. Trimethylhydrazine (CAS 1741-01-1); 5. Tetramethylhydrazine (CAS 6415-12-9); 6. N,N diallylhydrazine; 7. Allylhydrazine (CAS 7422-78-8); 8. Ethylene dihydrazine; 9. Monomethylhydrazine dinitrate; 10. Unsymmetrical dimethylhydrazine nitrate; 11. Hydrazinium azide (CAS 14546-44-2); 12. Dimethylhydrazinium azide; 13. Hydrazinium dinitrate; 14. Diimido oxalic acid dihydrazine (CAS 3457-37-2); 15. 2-hydroxyethylhydrazine nitrate (HEHN); 16. Hydrazinium perchlorate (CAS 27978-54-7); 17. Hydrazinium diperchlorate (CAS 13812-39-0); 18. Methylhydrazine nitrate (MHN); 19. Diethylhydrazine nitrate (DEHN); 20. 3,6-dihydrazino tetrazine nitrate (DHTN); c. Spherical or spheroidal aluminium powder (CAS 7429-90-5) in particle size of less than 200 x 10 -6 m (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; d. Metal powders of any of the following: zirconium (CAS 7440-67-7), beryllium (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, 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, consisting of 97% by weight or more of any of the above mentioned metals; Note: In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled. e. Metal powders of either boron (CAS 7740-42-8) 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; Note: In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled. f. High energy density materials, usable in the systems specified in 1.A. or 19.A., as follows: 1. Mixed fuels that incorporate both solid and liquid fuels, such as boron slurry, having a mass- based energy density of 40 x 10 6 J/kg or greater; 2. Other high energy density fuels and fuel additives (e.g., cubane, ionic solutions, JP-10) having a volume-based energy density of 37.5 x 10 9 J/m 3 or greater, measured at 20 o C and one atmosphere (101.325 kPa) pressure.
Authority: GBProhibited Supply To: IRProgram: UK-INUFuel substances as follows: a. Hydrazine (CAS 302-01 - 2) with a concentration of more than 70%; b. Hydrazine derivatives as follows: 1. Monomethylhydrazine (MMH) (CAS 60-34 - 4); 2. Unsymmetrical dimethylhydrazine (UDMH) (CAS 57-14-7); 3. Hydrazine mononitrate; 4. Trimethylhydrazine (CAS 1741-01-1); 5. Tetramethylhydrazine (CAS 6415-12-9); 6. N,N diallylhydrazine; 7. Allylhydrazine (CAS 7422-78-8); 8. Ethylene dihydrazine; 9. Monomethylhydrazine dinitrate; 10. Unsymmetrical dimethylhydrazine nitrate; 11. Hydrazinium azide (CAS 14546-44-2); 12. Dimethylhydrazinium azide; 13. Hydrazinium dinitrate; 14. Diimido oxalic acid dihydrazine (CAS 3457-37-2); 15. 2-hydroxyethylhydrazine nitrate (HEHN); 16. Hydrazinium perchlorate (CAS 27978-54-7); 17. Hydrazinium diperchlorate (CAS 13812-39-0); 18. Methylhydrazine nitrate (MHN); 19. Diethylhydrazine nitrate (DEHN); 20. 3,6-dihydrazino tetrazine nitrate (DHTN); c. Spherical or spheroidal aluminium powder (CAS 7429-90-5) in particle size of less than 200 x 10 -6 m (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; d. Metal powders of any of the following: zirconium (CAS 7440-67-7), beryllium (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, 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, consisting of 97% by weight or more of any of the above mentioned metals; Note: In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled. e. Metal powders of either boron (CAS 7740-42-8) 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; Note: In a multimodal particle distribution (e.g. mixtures of different grain sizes) in which one or more modes are controlled, the entire powder mixture is controlled. f. High energy density materials, usable in the systems specified in 1.A. or 19.A., as follows: 1. Mixed fuels that incorporate both solid and liquid fuels, such as boron slurry, having a mass- based energy density of 40 x 10 6 J/kg or greater; 2. Other high energy density fuels and fuel additives (e.g., cubane, ionic solutions, JP-10) having a volume-based energy density of 37.5 x 10 9 J/m 3 or greater, measured at 20 o C and one atmosphere (101.325 kPa) pressure.
Authority: GBProhibited Supply To: IRProgram: UK-INUComposite and composite modified double base propellants.
Authority: GBProhibited Supply To: IRProgram: UK-INUComposite and composite modified double base propellants.
Authority: GBProhibited Supply To: IRProgram: UK-INUEquipment as follows, and specially designed components therefor: a. 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: 1. A total volumetric capacity of 110 litres or more; and b. 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: 1. Two or more mixing/kneading shafts; or 2. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber; c. Fluid energy mills usable for grinding or milling substances specified in 4.C.; d. Metal powder “production equipment” usable for the “production”, in a controlled environment, of spherical or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e. 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).
Authority: GBProhibited Supply To: IRProgram: UK-INUEquipment as follows, and specially designed components therefor: a. 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: 1. A total volumetric capacity of 110 litres or more; and b. 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: 1. Two or more mixing/kneading shafts; or 2. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber; c. Fluid energy mills usable for grinding or milling substances specified in 4.C.; d. Metal powder “production equipment” usable for the “production”, in a controlled environment, of spherical or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e. 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).
Authority: GBProhibited Supply To: IRProgram: UK-INU