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2 084 677

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Application

94044773/06, 1994-12-20

(22)

Actual filing date

1994-12-20

(45)

Published

1997-07-20

(72)

Inventor

Klepikov Igor' AlekseevichBakhmutov Arkadij AlekseevichBukanov Vladislav TimofeevichKanalin Jurij IvanovichPrishchepa Vladimir Iosifovich

(73)

Holder

Klepikov Igor' AlekseevichBakhmutov Arkadij AlekseevichBukanov Vladislav TimofeevichKanalin Jurij IvanovichPrishchepa Vladimir Iosifovich

METHOD OF STARTING LIQUID ROCKET ENGINE AND LIQUID ROCKET ENGINE Russian patent published in 1997 - IPC

Abstract RU 2084677 C1

FIELD: rocket engineering. SUBSTANCE: method comprises supplying fuel components to the engine path and compressed starting gas to the turbine of the booster fuel pump. The liquid rocket engine comprises jet chamber, actuating turbine and pump, and lines for gas and liquid fuel components. The main supply pipe line for the booster turbine is provided with a branch pipe for connecting the actuating booster turbine with a source of compressed starting gas. EFFECT: simplified method and engine. 2 cl, 1 dwg

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RU 2 084 677 C1

Authors

Klepikov Igor' Alekseevich

Bakhmutov Arkadij Alekseevich

Bukanov Vladislav Timofeevich

Kanalin Jurij Ivanovich

Prishchepa Vladimir Iosifovich

Dates

1997-07-20—Published

1994-12-20—Filed

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