ROCKET Russian patent published in 2010 - IPC F42B15/00 

Abstract RU 2399865 C1

FIELD: weapons and ammunition.

SUBSTANCE: proposed rocket comprises sustainer stage, separable booster stage, staging mechanism with gas generator, primer, drive and striker. Drive is fixed in engine head part and furnished with piston with obturator on combustion chamber side and cylindrical hammer with flat end face on gas generator side. Gas generator is secured on sustainer stage opposite the drive striker. Gas generator bottom incorporates safety-actuator mechanism arranged on drive side and representing a sleeve with cylindrical space and central bore. Piston is arranged inside the sleeve to axially move therein. Striker is arranged on aforesaid piston on primer side, while cylindrical ledge aligned with striker is arranged is arranged on hammer side that enters the sleeve central bore on striker side.

EFFECT: higher reliability of rocket due to ruling out violation of production specs and random failures of structural elements.

3 dwg

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RU 2 399 865 C1

Authors

Kolikov Vladimir Anatol'Evich

Korennoj Aleksandr Vladimirovich

Morozov Valerij Dmitrievich

Savin Sergej Anatol'Evich

Surnachev Aleksandr Fedorovich

Vasina Elena Anatol'Evna

Dates

2010-09-20Published

2009-05-14Filed