首页> 外国专利> GYRATING ROCKET STAGE WITH COMBINED POWER PLANT AND METHOD OF CONTROLLING ROCKET FLIGHT

GYRATING ROCKET STAGE WITH COMBINED POWER PLANT AND METHOD OF CONTROLLING ROCKET FLIGHT

机译：联合电站旋转火箭弹的研制及控制火箭飞行的方法

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摘要

FIELD: transport.;SUBSTANCE: invention relates to rocketry. Gyrating stage comprises nose section and gas generator with pushing, pulling and bank control nozzles. Additionally, said stage comprises sustainer communicated via gas dust and bypass valve with gas generator. Sustainer incorporates thrust vector controls and represents solid propellant engine like gas generator. Gas generator solid propellant charge is made up of cylinder with central bore, its inner and outer surfaces being armored. Gas generator pressure is increased in combustion products overflowing from sustainer. Note here that sustainer and gas generator pressure and charge combustion rate exponents obey definite laws.;EFFECT: higher maneuverability and efficiency.;6 cl, 3 dwg

机译：技术领域本发明涉及火箭技术。回转级包括机头部分和带有推，拉和倾斜控制喷嘴的气体发生器。另外，所述级包括经由气体灰尘和旁通阀与气体发生器连通的保持器。 Sustainer整合了推力矢量控制，代表了固体推进剂发动机（如气体发生器）。气体发生器固体推进剂装药由带有中心孔的圆柱体组成，其内外表面均装有铠装。从支座溢出的燃烧产物中的气体发生器压力增加。请注意，维持器和气体发生器的压力和充气燃烧率指数服从确定定律。效果：更高的可操纵性和效率。6 cl，3 dwg

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公开/公告号RU2427507C1

专利类型
公开/公告日2011-08-27

原文格式PDF
申请/专利权人 FEDERALNOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATELNOE UCHREZHDENIE VYSSHEGO PROFESSIONALNOGO OBRAZOVANIJA IZHEVSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET;
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申请/专利号RU20100131988
发明设计人 SERMJAGIN KONSTANTIN VIKTOROVICH;ALIEV ALI VEJSOVICH;LOSHKAREV ANATOLIJ NIKOLAEVICH;MIRONOV ANDREJ NIKOLAEVICH;
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申请日2010-07-29
分类号B64G1/40;F42B10/40;
国家 RU
入库时间 2022-08-21 17:48:18

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