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《Missiles and Space Vehicles》 2012-01
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Fundamental Research on System Scheme of Next-generation High Thrust LOX/LH_2 Rocket Engine

Zheng Dayong,Zhang Weihong,Shi Wenliang(Beijing Aerospace Propulsion Institute,Beijing,100076)  
Aiming at current requirement of engine for the next-generation launch vehicle,suggestion of developing a new high thrust LOX/LH2 rocket engine is brought forward,and the fundamental research on power cycle,engine performance,transient character and reliability are conducted.The result indicates that the engine with high reliability,low production cost and appropriate performance is in accordance with the technical trend of future cryogenic LOX/LH2 engine.
【CateGory Index】: V434
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