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
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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 |
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代理人 |
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主权项 |
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地址 |
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