Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p242
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 689892–692971

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.
9. A. 111. Pulse jet or detonation engines usable in "missiles" or unmanned aerial vehicles specified by 9A012, and specially designed components therefor.
Technical Note:
In 9A111, detonation engines utilise detonation to produce a rise in effective pressure across the combustion chamber. Examples of detonation engines include pulse detonation engines, rotating detonation engines or continuous wave detonation engines.
N.B.: SEE ALSO 9A011 AND 9A118.
9. A. 112. "Unmanned aerial vehicles" ("UAVs"), other than those specified by 9A012, as follows:
a. "Unmanned aerial vehicles" ("UAVs") capable of a range of 300 km;
b. "Unmanned aerial vehicles" ("UAVs") having all of the following:
1. Having any of the following:
a. An autonomous flight control and navigation capability; or
b. Capability of controlled flight out of the direct vision range involving a human operator; and
9. A. 112. b. 2. Having any of the following:
a. Incorporating an aerosol dispensing system/mechanism with a capacity greater than 20 litres; or
b. Designed or modified to incorporate an aerosol dispensing system/mechanism with a capacity greater than 20 litres.
Technical Notes:
1. An aerosol consists of particulate or liquids other than fuel components, by products or additives, as part of the payload to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding.
2. An aerosol dispensing system/mechanism contains all those devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapour and into the propeller slip stream.
Note: Certain items specified in 9A112 may be subject to the MTCR Guidelines for Sensitive Missile‑Relevant Transfers.
9. A. 115. Launch support equipment as follows:

            1. Apparatus and devices for handling, control, activation or launching, designed or modified for space launch vehicles specified by 9A004, unmanned aerial vehicles capable of a range exceeding 300 km or sounding rockets specified by 9A104;

                  Note: Apparatus and devices specified in 9A115.a include those installed on a manned aircraft or an unmanned aerial vehicle.

b. Vehicles for transport, handling, control, activation or launching, designed or modified for space launch vehicles specified by 9A004 or sounding rockets specified by 9A104.
9. A. 116. 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.
9. A. 117. Staging mechanisms, separation mechanisms,