Deflection of exhaust gas stream (jet vanes or probes); or
5.
Thrust tabs.
9A109
Hybrid rocket motors and specially designed components as follows:
a.
Hybrid rocket motors usable in complete rocket systems or unmanned aerial vehicles, capable of 300 km, other than those specified in 9A009, having a total impulse capacity equal to or greater than 0,841 MNs, and specially designed components therefor;
b.
Specially designed components for hybrid rocket motors specified in 9A009 that are usable in "missiles".
N.B.: SEE ALSO 9A009 and 9A119.
9A110
Composite structures, laminates and manufactures thereof, other than those specified in 9A010, specially designed for use in 'missiles' or the subsystems specified in 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
N.B.: SEE ALSO 1A002.
Technical Note:
In 9A110 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
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
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".
N.B.: See also 9A121.
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: In 9A120 'other liquid propellants' includes, but is not limited to, propellants specified in the Military Goods Controls.
9A121
Umbilical and interstage electrical connectors specially designed for "missiles", space launch vehicles specified in 9A004 or sounding rockets specified in 9A104.
Technical Note:
Interstage connectors referred to in 9A121 also include electrical connectors installed between the "missile", space launch vehicle or sounding rocket and their payload.
9A350
Spraying or fogging systems, specially designed or modified for fitting to aircraft, "lighter-than-air vehicles" or unmanned aerial vehicles, and specially designed components therefor, as follows:
a.
Complete spraying or fogging systems capable of delivering, from a liquid suspension, an