Sunday, 1 November 2026
Standing Office 81 (SOVNPA 81) emblem Viet Nam NVietnam National Presiding Agency
on Countering the Proliferation of Weapons of Mass Destruction
Standing Office 81

9A108Components, other than those specified in 9A008, as follows, specially designed for solid and hybrid rocket propulsion systems:

List
EU dual-use list – Annex I to Regulation (EU) 2021/821, updated annually
Originating regime
MTCR
a. Rocket motor cases and insulation components therefor, usable in subsystems specified in 9A007, 9A009, 9A107 or 9A109.a.;
N.B. For insulation material in bulk or sheet form, SEE ALSO 9C108.
Note:
In 9A108, insulation intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps.
b. Rocket nozzles, usable in subsystems specified in 9A007, 9A009, 9A107 or 9A109.a.;
c. Thrust vector control sub-systems, usable in "missiles".
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.