MULTISTAGE ROCKET Russian patent published in 1997 - IPC

Abstract RU 2088787 C1

FIELD: rocketry; designing space launch vehicles. SUBSTANCE: rocket includes stages of tandem arrangement with oxidizer and fuel tanks, rocket engines, service pipe lines and stage separation devices. Engine of subsequent stage is immersed in propellant tank of previous stage under common bottom; lateral wall of this tank forms housing of engine bay of subsequent stage which is separable in flight. EFFECT: enhanced reliability. 1 dwg

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RU 2 088 787 C1

Authors

Bakhmutov Arkadij Alekseevich

Klepikov Igor' Alekseevich

Prishchepa Vladimir Iosifovich

Dates

1997-08-27Published

1994-03-28Filed