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

Abstract RU 2399564 C1

FIELD: transport.

SUBSTANCE: invention relates to aerospace engineering. Proposed engine plant comprises engine fuel and oxidiser tanks to supply sustainer engine, high-pressure cylinder to supply gas for engine plant actuators, pressure reducer communicated via pipeline with high-pressure cylinder to create operating pressure at the inlets of actuators. Additionally, pipeline is added to engine plant, with its inlet communicated with pressure reducer drain union, while its outlet Y-tube added to fuel tank pressurisation pipeline.

EFFECT: improved weight dimension characteristics of rocket unit.

1 dwg

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RU 2 399 564 C1

Authors

Erpylev Vladimir Vladimirovich

Rozhkov Mikhail Viktorovich

Dates

2010-09-20—Published

2009-04-13—Filed