ROCKET NOSE CONE Russian patent published in 2000 - IPC

Abstract RU 2151363 C1

FIELD: rocketry. SUBSTANCE: spin-stabilized rocket nose has a nose fairing with a dropping device and a multiple parachute system with shroud lines attached to the rocket. The parachute canopies packed in separate sleeves are located in the nose fairing with a shift relative to the rocket spin axis. EFFECT: enhanced reliability of actuation of rocket parachute system. 3 cl, 1 dwg

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RU 2 151 363 C1

Authors

Sokolovskij M.I.

Bondarenko S.A.

Zykov G.A.

Shein A.G.

Dates

2000-06-20—Published

1999-02-08—Filed