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2 065 985

(13)

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IPC

(21) (22)

Application

94029116/06, 1994-08-03

(22)

Actual filing date

1994-08-03

(45)

Published

1996-08-27

(72)

Inventor

Goncharov N.S.Lipljavyj I.V.Orlov V.A.Plis A.G.Rachuk V.S.Chembartsev S.V.Shostak A.V.

(73)

Holder

Kb Khimavtomatiki G.Voronezh

THREE-COMPONENT LIQUID-FUEL ROCKET ENGINE Russian patent published in 1996 - IPC

Abstract RU 2065985 C1

FIELD: rocket engineering. SUBSTANCE: engine has three-component gas generator connected through automatic control and regulation apparatus with first-fuel pump and through manifold - with second-fuel line. Connected to first-fuel feed line is inert gas purging trunk line. First-fuel pump is mounted on common shaft with additional second- fuel pump. Turbines of three turbine-driven pumps are supplied with generator- produced gas through three-way valve which is switched for engine operation with two-component fuel. EFFECT: high efficiency. 1 cl, 1 dwg

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RU 2 065 985 C1

Authors

Goncharov N.S.

Lipljavyj I.V.

Orlov V.A.

Plis A.G.

Rachuk V.S.

Chembartsev S.V.

Shostak A.V.

Dates

1996-08-27—Published

1994-08-03—Filed