FIELD: weapons.
SUBSTANCE: hydrid ballistic cruise rocket (BCR) comprises separable tail part, i.e. ballistic rocket, and warhead. The latter represents a cruise missile (CM) with engine for independent flight towards the target. BCR incorporates rocket engine with its nozzle directed opposite BCR flight. Antiwing with controlled angle of attack is arranged in the nozzle gas flow to change BCR in decelerated descent conditions.
EFFECT: higher efficiency.
1 dwg
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RU2752730C1 |
