| 发明名称 |
AERO-SPACE SYSTEM |
| 摘要 |
aeronautical and space engineering. SUBSTANCE: system includes aircraft, vertical cryogenic reservoir filled with liquid oxygen and space launch vehicle with liquid-propellant engine plant of first stage provided with liquid oxygen tank and drainage valves, pipe lines and pump used for preparation of air start from aircraft fuselage. Front portion of tank is provided with splitter plate having hole for forming closed gas-and-liquid cavity and liquid cavity whose upper portion is connected with upper portion of reservoir. EFFECT: enhanced reliability of start of engine plant of first stage of launch vehicle. 4 dwg
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| 申请公布号 |
RU2165869(C1) |
申请公布日期 |
2001.04.27 |
| 申请号 |
RU20000120655 |
申请日期 |
2000.08.08 |
| 申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "RAKETNO-KOSMICH;RAKETNO KOSM AOOT |
发明人 |
BORISENKO A.A.;DENISOV A.V.;EGOROV A.M.;ZAKHAROV S.N.;KIRSANOV G.V.;KLIPPA V.P.;LUK'JANOVA EH.A.;MARK V.A.;MILAKOV V.V.;PETROV N.K.;POPOV K.K.;PODOBEDOV G.G.;SERDJUK A.A.;SYROVETS M.N.;TUPITSYN N.N.;FEDOROV V.I.;FILIN V.M.;KHASPEKOV V.G.;SHAKHOV V.N. |
| 分类号 |
B64G1/14;(IPC1-7):B64G1/14 |
主分类号 |
B64G1/14 |
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