MULTI-STAGE ROCKET Russian patent published in 1997 - IPC

Abstract RU 2086795 C1

FIELD: rocketry; multi-stage liquid-propellant rockets. SUBSTANCE: multi-stage rocket comprises tandem stage with separation devices, rocket engines and tanks for liquid propellant components. Tank of previous stage of one propellant component is divided into front and rear sections by tank of other component; engine of subsequent stage is sunk in first section; provision is made for devices for communication with surrounding medium. EFFECT: reduction of power requirements for control of flight and structural mass. 2 cl, 1 dwg

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RU 2 086 795 C1

Authors

Bakhmutov Arkadij Alekseevich

Klepikov Igor' Alekseevich

Obukhov Nikolaj Aleksandrovich

Mogilenko Vladimir Ivanovich

Dates

1997-08-10Published

1994-09-27Filed