ROCKET ENGINE UNIT Russian patent published in 2010 - IPC F02K9/42 B64G1/40

Abstract RU 2381378 C1

FIELD: engines and pumps.

SUBSTANCE: invention relates to rocketry and can be used in designing rocker carrier first stages with multi-tank propellant compartments with wrap-around arrangement. Engine unit comprises multi-tank propellant compartment and fluid propellant rocket engines, every engine being communicated, via feed lines, with adjoining tanks. One of the engines communicates, via feed lines and booster pump units, with all tanks.

EFFECT: synchronised utilisation of propellant components from like tanks without introducing disturbing torques to rocket.

1 cl, 1 dwg

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RU 2 381 378 C1

Authors

Dresvjannikov Vasilij Ivanovich

Oparin Jurij Afanas'Evich

Dates

2010-02-10—Published

2008-07-24—Filed