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LOX/LCH_4变推力发动机技术初步研究
引用本文:刘昌波,李福云,兰晓辉,林革.LOX/LCH_4变推力发动机技术初步研究[J].火箭推进,2010,36(1):25-32.
作者姓名:刘昌波  李福云  兰晓辉  林革
作者单位:西安航天动力研究所,陕西,西安,710100
摘    要:对国内外变推力发动机和LOX/LCH4发动机的研究进展进行了总结,在此基础上,提出了一种LOX/LCH4变推力发动机系统方案。在深入分析的基础上,对此方案进行了功率平衡和推力室传热计算,结果表明该系统方案完全能够实现10:1推力变比。LOX/LCH4变推力发动机可以广泛应用于多种运载器和航天器中,对我国探月及后续的载人登月工程均可以提供技术支持,对LOX/LCH4发动机的技术发展和未来的载人登陆火星等任务都具有深远影响。

关 键 词:LOX/LCH4  膨胀循环  变推力  火箭发动机

Conceptual investigation on a LOX/LCH4 deep throttling rocket engine
Liu Changbo,Li Fuyun,Lan Xiaohui,Lin Ge.Conceptual investigation on a LOX/LCH4 deep throttling rocket engine[J].Journal of Rocket Propulsion,2010,36(1):25-32.
Authors:Liu Changbo  Li Fuyun  Lan Xiaohui  Lin Ge
Institution:(Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)
Abstract:This paper summarizes the status of deep throttling rocket engines and LOX/LCH4 rocket engines. A scheme of LOX/LCH4 deep throttling rocket engine is discussed. The power balance and heat transfer are computed based on careful analysis. The results show that the engine can throttle from 100% to 10% in thrust. LOX/LCH4 deep throttling rocket engine could be widely used in variety launch vehicles and spacecrafts, and be helpful to future China Lunar Exploration Program and Manned Lunar Plan and be beneficial to technologies of LOX/LCH4 liquid rocket engines and future Manned Mars.
Keywords:LOX/LCH4
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