首页> 外国专利> METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF FUEL AND OXYGEN OXIDIZER AND LIQUID-PROPELLANT ROCKET ENGINE FOR IMPLEMENTING SAID METHOD

METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF FUEL AND OXYGEN OXIDIZER AND LIQUID-PROPELLANT ROCKET ENGINE FOR IMPLEMENTING SAID METHOD

机译：以燃料和氧气增氧剂为基础的液化火箭发动机的涡轮增压低温燃料推进剂的操作方法

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FIELD: rocketry. SUBSTANCE: according to proposed method of operation of liquidpropellant rocket engine with turbopump delivery of cryogenic propellant on basis of oxygen oxidizer and fuel, recovering gas, after generation of vapor, is used directly for afterburning in chamber with remaining part of fuel. Liquid propellant rocket engine implementing proposed method employs gas generator designed for generating recovering gas being connected directly to nozzle head of chamber. EFFECT: increased efficiency of liquid-propellant rocket engine by increasing specific thrust pulse. 5 cl, 3 dwg

机译：领域：火箭。物质：根据提议的操作方法，在氧气氧化剂和燃料的基础上，涡轮泵输送低温推进剂的涡轮泵输送低温推进剂，在产生蒸汽之后，回收气体直接用于在燃烧室内燃烧余下的燃料。实现所提出的方法的液体推进剂火箭发动机采用了被设计为产生回收气体的气体发生器，该气体发生器被直接连接到腔室的喷嘴头。效果：通过增加比推力脉冲来提高液体推进剂火箭发动机的效率。 5厘升，3公升

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公开/公告号RU2197629C2

专利类型
公开/公告日2003-01-27

原文格式PDF
申请/专利权人 BAKHMUTOV ARKADIJ ALEKSEEVICH;BUKANOV VLADISLAV TIMOFEEVICH;KLEPIKOV IGOR ALEKSEEVICH;MIROSHKIN VJACHESLAV VASILEVICH;PRISHCHEPA VLADIMIR IOSIFOVICH;ROMASENKO TATJANA JAKOVLEVNA;
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申请/专利号RU20010107629
发明设计人 MIROSHKIN V.V.;ROMASENKO T.JA.;BAKHMUTOV A.A.;BUKANOV V.T.;KLEPIKOV I.A.;PRISHCHEPA V.I.;
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申请日2001-03-26
分类号F02K9/48;
国家 RU
入库时间 2022-08-21 23:44:01

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