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.
9A107
Solid propellant rocket engines, usable in complete rocket systems or unmanned aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, having total impulse capacity equal to or greater than 0,841 MNs.
N.B.: SEE ALSO 9A119.
9A108
Components, other than those specified in 9A008, 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 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.
Technical note:
In 9A109 "missile" means complete rockets system and unmanned aerial vehicle systems capable of a range exceeding 300 km.
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" or unmanned aerial vehicles specified in 9A012, and specially designed components therefor.
N.B.: SEE ALSO 9A011 AND 9A118.
9A115
Launch support equipment as follows:
a.
apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004, unmanned aerial vehicles specified in 9A012 or sounding rockets specified in 9A104;
b.
vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
9A116
Re-entry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows:
a.
re-entry 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 re-entry vehicles.
9A117
Staging mechanisms, separation mechanisms, and interstages, usable in "missiles".
9A118
Devices to regulate combustion usable in engines, which are usable in "missiles" or unmanned aerial vehicles specified in 9A012, specified in 9A011 or 9A111.
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 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109.
9A120
Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 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: