航天推进技术研究院主办
[1]张蒙正,南向谊,刘典多.预冷空气涡轮火箭组合动力系统原理与实现途径[J].火箭推进,2016,42(01):6-12.
ZHANG Mengzheng,NAN Xiangyi,LIU Dianduo.Principles and realizing ways of combined power system for pre-cooling air turbo rocket[J].Journal of Rocket Propulsion,2016,42(01):6-12.
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ZHANG Mengzheng,NAN Xiangyi,LIU Dianduo.Principles and realizing ways of combined power system for pre-cooling air turbo rocket[J].Journal of Rocket Propulsion,2016,42(01):6-12.
预冷空气涡轮火箭组合动力系统原理与实现途径
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
42
期数:
2016年01期
页码:
6-12
栏目:
专论与综述
出版日期:
2016-04-01
- Title:
- Principles and realizing ways of combined power system for pre-cooling air turbo rocket
- Keywords:
- pre-cooling air turbo rocket; key technology; realizing way
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 针对重复使用航天运输系统及临近空间快速投放平台动力需求,提出了一种预冷空气涡轮火箭组合动力系统方案,分析了此动力系统的技术特点及与其他组合循环动力的差异,进行了系统初步性能分析.研究表明:通过调节系统参数,此动力系统参数闭合,性能较佳,方案可行;进一步分析了动力系统涉及的核心技术及技术基础,认为预冷空气涡轮火箭组合动力系统具有可实现性.
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更新日期/Last Update:
1900-01-01