ADJUSTABLE LIQUID ROCKET ENGINE

The invention relates to rocket engineering, more specifically to rocket engines using liquid fuel components. The inventive liquid rocket engine comprises a chamber (1), a gas generator (2), a pump-turbine unit provided with centrifugal pumps (6,7,8), a turbine (5) and an automatic system provided...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CHVANOV, VLADIMIR KONSTANTINOVICH, KIRILLOV, VICTOR VASILIEVICH, LACHINOV, DMITRY SERGEEVICH, ANTIPOV, YURY SERGEEVICH, FEDORCHENKO, ALEXANDER VLADIMIROVICH, TYURIN, ALEXANDER ANATOLYEVICH, SEMENOV, VADIM ILIYCH, TELENKOV, ALEXANDER ALEXEEVICH, GROMYKO, BORIS MIKHAILOVICH, STOROZHENKO, IGOR GRIGORIEVICH, KATORGIN, BORIS IVANOVICH, KIRILLOV, ALEXEY VICTOROVICH
Format:	Patent
Sprache:	eng ; fre ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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