4.Solid Propellant and Propellant Constituents

(1) Metal fuels with particle sizes less than 500 mm, whether spherical, atomized, spheroidal, flaked or ground, consisting of 97 percent by weight or greater of any of the following metal and alloys of these:

(a) Zirconium;

(b) Boron;

(c) Magnesium;

(d) Titanium;

(e) Uranium;

(f) Tungsten;

(g) Zinc;

(h) Cerium.

(2) Ammonium perchlorate with particle sizes less than 500 mm;

(3) Spherical aluminum powder meeting the following requirements:

(a) With particle of uniform diameter;

(b) With aluminum content of 97 percent or greater;

(c) With diameter of less than 500 mm.

(4) Boron Slurry, having an energy density of more than 40 x 106 J/kg;

(5) Nitro-amines:

(a) Cyclotetramethylene-tetranitramene (HMX);

(b) Cyclotrimethylene-trinitramine (RDX).

(6) Composite Propellants:

(a) Molded colloid propellants;

(b) Propellant including nitrate bonding agents and with an aluminum (particle) content of 5 percent or greater.

(7) Polymeric substances:

(a) Carboxl-terminated polybutadiene (CTPB);

(b) Hydroxy-terminated polybutadiene (HTPB).

(8) Triethylamine as an igniting agent.

5.Guidance and Control Set, Components and Related Technologies

(1) Gyro-astro compasses and other devices which derive position or orientation by means of automatically tracking celestrial bodies or satellites;

(2) Flight control software and related test software;

(3) Gyro stability platform;

(4) Automatic pilots for UAV;

(5) Gyros with a rated drift rate stability of less than 0.5 degree per hour;

(6) Test table for inertial platform (including high-accuracy centrifuges and rotating table);

(7) Inertial Measurement Unit (IMU) tester;

(8) Inertial Measurement Unit (IMU) stable element handling fixture;

(9) Inertial Measurement Unit (IMU) platform balance fixture;

(10) Tester for gyro tuning;

(11) Tester for gyro dynamic balance;

(12) Gyro run-in/motor test station;

(13) Gyro evacuation and filling station;

(14) Centrifuge fixture for gyro bearings;

(15) Rectangular scatterometer for ring laser gyro production;

(16) Polarity scatterometer for ring laser gyro production;

(17) Reflectometer for ring laser gyro production;

(18) Surface profilometer for ring laser gyro production;

(19) Accelerometers with a proportional error of 0.25 percent or less;

(20) Accelerometer test station;

(21) Accelerometer axis align station;

(22) Specially designed test, calibration, and alignment equipment for gyro or accelerometer.

6.Target Detection System and Related Electronics

(1) Radar systems;

(2) Altimeters;

(3) Terrain contour mapping equipment;

(4) Scene mapping and correlation (both digital and analog) equipment;

(5) Imaging sensor equipment;

(6) Processors and software specially designed for processing navigation information;

(7) Electronic devices and components removed of conductive heat;

(8) Radiation-hardened electronic devices and components;

(9) Electronic assemblies and components operating at temperatures in excess of 125 °C for a short period of time;

(10)Electronic devices and components with specially designed integrated support;

(11) Telemetry equipment and related technologies;

(12) Telemetering and telecontrol ground equipment;

(13) Analogue computers and digital computers having either of the following characteristics:

(a) Rated for continuous operation at temperatures from below minus 45 °C to above plus 55 °C;

(b) Designed as ruggedized or radiation hardened.

(14) Analogue-to-digital converter having one of the following characteristics:

(a) Rated for operation at temperatures from below minus 54 °C to above plus 125 °C, and

(b) Designed to meet military specifications for ruggedized equipment; or

(c) Designed or modified for military use or designed as radiation hardened, and having one of the following characteristics:

① Converting at a rate of over 200000 times (complete conversion) per second under rated accuracy;

② With accuracy exceeding 1/10000 of the whole range in the rated temperature scope;

③With quality factor of over 1′108 (complete conversion times per second divided by accuracy);

④The inbuilt microcircuits having the following characteristics:

(A) The maximum converting time is less than 20 microseconds under maximum resolution, and

(B) The rated nonlinearity is better than 0.025 percent of the range in rated temperature scope.

(15) Design technology for protection of avionics and electrical subsystems against electromagnetic pulse and electromagnetic interference hazards from external sources:

(a) Design technology for shielding systems;

(b) Design technology for the configuration of hardened electrical circuits and subsystems;

(c) Determination of hardening criteria for the above.

7.Material

(1) Structural composites, including composite structures, laminates, and manufactures thereof, and resin impregnated fibre prepregs and metal coated fibre preforms therefor, made with either organic matrix or metal matrix utilizing fibrous or filamentary reinforcements having a specific tensile strength greater than 7.62 x 104 m and a specific modulus greater than 3.18 x 106 m:

(a) Polyimide composite;

(b) Polyamide composite;

(c) Polycarbonate composite;

(d) Quartz-fibre-reinforced composite;

(e) Carbon-fibre-reinforced composite;

(f) Boron-fibre-reinforced composite;

(g) Magnesium matrix composite;

(h) Titanium matrix composite.

(2) Ceramic composite materials with dielectric constant less than 6 at frequencies from 100 Hz to 10,000 MHz;

(3) Fine grain bulk artificial graphites having the following features measured at 20 °C:

(a) With a bulk density of at least 1.72 g/cm3;

(b) With a tension rupture strain of at least 0.7 percent;

(c) With a heat expansion coefficient of at least 2.75′10-6 (measured at temperatures from 20 °C to 982 °C).

(4) Resaturated pyrolized carbon-carbon materials;

(5) Special Steel:

Titanium-stabilized duplex stainless steel (Ti-DSS) having the following characteristics:

(a) Containing 17.0 to 26.5 weight percent chromium and 4.5 to 7.0 weight percent nickel;

(b) Having a ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10 percent is austenite by volume;

(c) 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;

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

(6) Ceramic heat shielding material;

(7) Ablative heat shielding material.