9A008, usable in "missiles", as follows, specially designed for solid rocket propulsion systems:
a. Rocket motor cases, "interior lining" and "insulation" therefor;
b. Rocket nozzles;
c. Thrust vector control sub-systems.
Technical Note:
Examples of methods of achieving thrust vector control specified in 9A108.c. are:
1. Flexible nozzle;
2. Fluid or secondary gas injection;
3. Movable engine or nozzle;
4. Deflection of exhaust gas stream (jet vanes or probes); or
5. Thrust tabs.
9A109 Hybrid rocket motors, usable in "missiles", other than those specified in 9A009, and specially designed components therefor.
N.B.:
SEE ALSO 9A119.
9A110 Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 or the subsystems specified in 9A005, 9A007, 9A105.a., 9A106 to 9A108, 9A116 or 9A119.
N.B.:
SEE ALSO 1A002.
9A111 Pulse jet engines, usable in "missiles", and specially designed components therefor.
N.B.:
SEE ALSO 9A011 and 9A118.
9A115 Launch support equipment, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104, as follows:
a. Apparatus and devices for handling, control, activation or launching;
b. Vehicles for transport, handling, control, activation or launching.
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.
9A117 Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".
9A118 Devices to regulate combustion usable in engines, which are usable in "missiles", specified in 9A011 or 9A111.
9A119 Individual rocket stages, usable in complete rocket systems or unmanned air vehicles, capable of a range of 300 km, other than those specified in 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
9B Test, Inspection and Production Equipment
9B001 Specially designed equipment, tooling and fixtures, as follows, for manufacturing gas turbine blades, vanes or tip shroud castings:
a. Directional solidification or single crystal casting equipment;
b. Ceramic cores or shells;
9B002 On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for the "development" of gas turbine engines, assemblies or components incorporating "technologies" specified in 9E003.a.
9B003 Equipment specially designed for the "production" or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s, and temperatures in excess of 773 K (500 °C), and specially designed components or accessories therefor.
9B004 Tools, dies or fixtures for the solid state joining of "superalloy", titanium or intermetallic airfoil-to-disk combinations described in 9E003.a.3. or 9E003.a.6. for gas turbines.
9B005 On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following wind tunnels or devices:
N.B.:
SEE ALSO 9B105.
a. Wind tunnels designed for speeds of Mach 1,2 or more, except those specially designed for educational purposes and having a