发明名称 System for conditioning and igniting a rocket motor
摘要 A system for conditioning and providing power to receivers in a rocket motor, comprises a single torch (10) with hot core, means (11, 11a; 12, 12a) for selectively feeding the torch (10) with ergols contained in tanks (1, 2) associated with the rocket motor, at least one heat exchanger (23, 26) for providing a heat exchange between the combustion gases (GC) coming from the torch (10) and a conditioning fluid circulating selectively in a heat conditioning circuit of functional members of the rocket motor to be heated up or cleansed, and means (66) for selectively applying the combustion gases (CG) from the torch (10) to at least one power receiver (53) such as the main ignition device of the main chamber (52) of the rocket motor. <IMAGE>
申请公布号 FR2671138(A1) 申请公布日期 1992.07.03
申请号 FR19900016513 申请日期 1990.12.28
申请人 PROPULSION STE EUROPEENNE 发明人 BEAURAIN ANDRE
分类号 B64G1/40;F02K9/95 主分类号 B64G1/40
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