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MULTISTAGED CRUISE MISSILE

机译:多级巡航导弹

摘要

FIELD: defense technology.;SUBSTANCE: multistaged cruise missile comprises at least two stages with engines and fuel and oxidant tanks connected to them by means of low pressure pipelines. Each engine comprises combustion chamber with system of regenerative cooling, turbopump set and gas generator. Turbopump set comprises oxidant and fuel pumps and main and startup turbine, and gas generator is installed coaxially with turbopump set. Outlet of fuel pump is connected to inlet of regenerative cooling system and to inlet of gas generator, outlet of oxidant pump is connected to the second inlet of gas generator, outlets of gas generator and system of regenerative cooling are connected to cylindrical portion of combustion chamber.;EFFECT: improved technical characteristics of missile in wide range of flight modes at various heights.;2 dwg
机译:领域:国防技术;实质:多级巡航导弹至少包括两级,发动机,燃料和氧化剂罐通过低压管道与之相连。每个发动机包括带有再生冷却系统的燃烧室,涡轮泵组和气体发生器。涡轮泵机组包括氧化剂和燃油泵以及主涡轮和启动涡轮,气体发生器与涡轮泵机组同轴安装。燃料泵的出口连接到再生冷却系统的入口和气体发生器的入口,氧化剂泵的出口连接到气体发生器的第二入口,气体发生器的出口和再生冷却的系统连接到燃烧室的圆柱形部分。;效果:在各种高度的各种飞行模式下改进的导弹技术特性; 2 dwg

著录项

  • 公开/公告号RU2380647C1

    专利类型

  • 公开/公告日2010-01-27

    原文格式PDF

  • 申请/专利权人 BOLOTIN NIKOLAJ BORISOVICH;

    申请/专利号RU20080144260

  • 发明设计人 BOLOTIN NIKOLAJ BORISOVICH;

    申请日2008-11-07

  • 分类号F42B15/00;

  • 国家 RU

  • 入库时间 2022-08-21 18:29:48

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