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2 125 176

(13)

C1

(51)

IPC

(21) (22)

Application

95120995/06, 1995-12-13

(22)

Actual filing date

1995-12-13

(45)

Published

1999-01-20

(72)

Inventor

Vinogradov V.N.Njatin A.G.

(73)

Holder

Opytnoe Konstruktorskoe Bjuro

COMPRESSED GAS PROPELLANT ROCKET ENGINE Russian patent published in 1999 - IPC

Abstract RU 2125176 C1

FIELD: spacecraft; gas reaction control systems of space vehicles. SUBSTANCE: rocket engine has pipeline, valve, gas dynamic throttle, heat exchanger, power control unit, and nozzle. Opening of valve provides delivery of gas throttle in which pressure is reduced and stabilized at required level, gas in heated in heat exchanger and ejected through nozzle, thus creating reactive thrust. EFFECT: increased accuracy of thrust control which is necessary for provision of high accuracy control of position of space vehicle. 1 dwg

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RU 2 125 176 C1

Authors

Vinogradov V.N.

Njatin A.G.

Dates

1999-01-20—Published

1995-12-13—Filed

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