固液推进技术在载人登月中的应用

朱浩; 田辉; 蔡国飙

固液推进技术在载人登月中的应用

北京航空航天大学宇航学院, 北京 100191

基金项目: 国家863基金资助项目(2010AA)

详细信息

中图分类号: V 436
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出版历程
- 收稿日期: 2011-12-21
- 网络出版日期: 2012-04-30

Application of hybrid rocket motor on manned lunar landing

School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 通过对世界主要航天国家和地区新世纪载人登月计划的研究、美国"阿波罗"飞船登月舱动力系统的详细分析,基于固液推进技术的特点,利用遗传算法开展了固液火箭发动机替代"阿波罗"登月舱下降级和上升级液体火箭发动机方案的优化设计,并对两者在功能、质量、体积和推进剂特性上进行了对比分析.结果表明固液推进技术在载人登月以及深空探测中具有良好的应用优势和前景.
- 固液推进技术 /
- 载人登月 /
- 优化设计
Abstract: A primary optimal design of manned lunar ship with hybrid propulsion system was proposed. After researching on the manned lunar plans of the main space industry countries and regions and analysis of "Apollo" lunar module, based on hybrid rocket motor system design model, a genetic arithmetic was used to optimize the hybrid rocket motors substituting the descent and ascent liquid rocket motors of "Apollo" lunar module. The comparison and analysis of their function, mass, volume and propellant characteristics show that it has great advantages and application prospect for hybrid propulsion technology to be used in manned lunar ship and deep space exploration.
- hybrid rocket motor /
- manned lunar landing /
- optimal design

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参考文献(12)

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