STAROVEROV'S-11 ROCKET ENGINE Russian patent published in 2014 - IPC F02K9/97 

Abstract RU 2505700 C1

FIELD: engines and pumps.

SUBSTANCE: rocket engine comprises housing and jet nozzle. Flange is made at jet nozzle end whereto tightly secured is the limited-durability cover. Engine housing accommodates nitrogen pentoxide and inert gas in amount of 0.0001-0.1% of fuel weight. Said inert gas represents xenon, krypton, argon, nitrogen and Freon-22. Said cover supports gas cylinder provided with filling union, pressure control valve and bypass valve.

EFFECT: better power characteristics.

1 dwg

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RU 2 505 700 C1

Authors

Staroverov Nikolaj Evgen'Evich

Dates

2014-01-27Published

2012-07-09Filed