发明名称 STAROVEROV'S-11 ROCKET ENGINE
摘要 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
申请公布号 RU2505700(C1) 申请公布日期 2014.01.27
申请号 RU20120128744 申请日期 2012.07.09
申请人 STAROVEROV NIKOLAJ EVGEN'EVICH 发明人 STAROVEROV NIKOLAJ EVGEN'EVICH
分类号 F02K9/97 主分类号 F02K9/97
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