航天推进技术研究院主办
[1]沈赤兵,李清廉,罗世彬,等.三组元火箭发动机推力室试验研究[J].火箭推进,2006,32(05):1-6.
Shen Chibing,Li Qinglian,Luo Shibin,et al.Experimental research on the thrust chamber of tripropellant rocket engine[J].Journal of Rocket Propulsion,2006,32(05):1-6.
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Shen Chibing,Li Qinglian,Luo Shibin,et al.Experimental research on the thrust chamber of tripropellant rocket engine[J].Journal of Rocket Propulsion,2006,32(05):1-6.
三组元火箭发动机推力室试验研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
32
期数:
2006年05期
页码:
1-6
栏目:
出版日期:
2006-10-30
- Title:
- Experimental research on the thrust chamber of tripropellant rocket engine
- 分类号:
- V431
- 文献标志码:
- A
- 摘要:
- 通过冷试研究了多种喷嘴的特性,总结了工作参数和结构参数对喷嘴性能的影响规律;进行了大量三组元推力室双工况热试,研究了不同工作参数和结构参数对三组元推力室燃烧性能的影响;利用旁通阀方案和液氧可调汽蚀文氏管方案分别成功进行了三组元工况与两组元工况的模态转换试验,实现了大范围工况调节;对三组元推力室内部燃烧和传热过程进行了数值仿真,考察了推力室冷却方案的可行性。
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备注/Memo
国家“863”基金;项目编号:203AA722011。
更新日期/Last Update:
1900-01-01