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2 076 229

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IPC

(21) (22)

Application

94035242/06, 1994-09-22

(22)

Actual filing date

1994-09-22

(45)

Published

1997-03-27

(72)

Inventor

Klepikov Igor' AlekseevichBakhmutov Arkadij AlekseevichKanalin Jurij IvanovichPrishchepa Vladimir Iosifovich

(73)

Holder

Klepikov Igor' AlekseevichBakhmutov Arkadij AlekseevichKanalin Jurij IvanovichPrishchepa Vladimir Iosifovich

ROCKET ENGINE FEED SYSTEM Russian patent published in 1997 - IPC

Abstract RU 2076229 C1

FIELD: rocket engines; feed systems of liquid-propellant rocket engines. SUBSTANCE: system includes main and booster turbopump units and pumps and drive gas turbines, gaseous working media generators, gas and liquid mains; inlet of booster turbine is brought in communication with gas line of generator and outlet is brought in communication with inlet of main pump. Mains of main and booster turbines may be brought in communication relative to each other; surface-type recuperative heat exchanger where cooling fuel component flows may be mounted between them. EFFECT: enhanced efficiency. 3 cl, 1 dwg

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RU 2 076 229 C1

Authors

Klepikov Igor' Alekseevich

Bakhmutov Arkadij Alekseevich

Kanalin Jurij Ivanovich

Prishchepa Vladimir Iosifovich

Dates

1997-03-27—Published

1994-09-22—Filed