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膨胀循环氢氧发动机低箱压起动特性研究

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为满足长时间在轨低温上面级对发动机低入口压力起动的需求,对膨胀循环氢氧发动机低箱压起动特性进行了仿真和试验研究,建立了较为准确的起动特性仿真模型,完成了地面环境和高空模拟环境氢入口低箱压起动试验.结果表明,氢入口压力越低,发动机起动加速性越慢,两者呈类似双曲线关系;降低喷管出口背压有利于发动机起动,氢入口压力越低,背压对起动加速性的影响越大.
Research on low-pressure start-up characteristics of expander cycle LOX/LH2 engine
In order to meet the demand for low inlet pressure start-up of the cryogenic upper stage,simulation and experimental research on the low tank pressure start-up characteristics of the expander cycle LOX/LH2 engine were conducted.An relatively accurate simulation model for start-up process was established,and the start-up tests of low hydrogen inlet pressure in both ground and simulated high altitude environment were completed.The results show that the start-up acceleration slows down with the decrease of hydrogen inlet pressure,which is similar to hyper-bolic relation.Reducing the back pressure at the nozzle outlet is beneficial to start-up,the lower the hydrogen inlet pressure,the greater the effect of back pressure on the starting acceleration.

expander cycle enginelow tank pressurestart-up characteristicsAMESim

李锦江、吴瑾清、孙慧娟、崔荣军、张楠

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北京航天动力研究所 北京 100076

中国航天科技集团有限公司低温液体推进技术实验室 北京 100076

膨胀循环发动机 低箱压 起动特性 AMESim

载人航天预先研究项目

050101

2024

低温工程
北京航天试验技术研究所

低温工程

CSTPCD北大核心
影响因子:0.568
ISSN:1000-6516
年,卷(期):2024.(2)
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