Aerospace and Propulsion
Hybrid rocket motors and specially designed components as follows:
| Reference | Parameter | Threshold |
|---|---|---|
| 9A109.a | having a total impulse capacity equal to or | > 0841 MNs |
| 9A109.a | having a total impulse capacity | >= 0841 MNs |
9A109.aHybrid 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;
9A109.bSpecially designed components for hybrid rocket motors specified in 9A009 that are usable in "missiles".
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