发明名称 PROPELLANT SUPPLY SYSTEM FOR SPACECRAFT ENGINE PLANT
摘要 space engineering. SUBSTANCE: system includes propellant tanks whose hydraulic cavities are connected with propellant supply manifold, start and shut-off valves and propellant tank pressurization system. Propellant feed system is provided with pups mounted in sections of mains between propellant tanks and start and shut-off valve separating hydraulic cavities of propellant tanks form propellant supply manifolds of jet engines. Low-pressure indicator is fitted in propellant supply mains before each pump; high-pressure indicator is fitted at pump outlet; these indicators are electrically connected with propellant supply system automatic control unit. EFFECT: reduced amount of high-pressure gas in propellant supply system of engine plant; improved mass and dimensional characteristics. 1 dwg
申请公布号 RU2189485(C2) 申请公布日期 2002.09.20
申请号 RU20000126941 申请日期 2000.10.26
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "RAKETNO-KOSMICH 发明人 GORELIKOV V.I.;OGNEV G.L.
分类号 F02K9/50 主分类号 F02K9/50
代理机构 代理人
主权项
地址