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[1]申智帅,等.气动增压器技术及其在空间推进系统的应用[J].火箭推进,2015,41(03):15-20.
　SHEN Zhi-shuai,RUAN Hai-jun,et al.Pneumopump technology and its application in space propulsion system[J].Journal of Rocket Propulsion,2015,41(03):15-20.
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气动增压器技术及其在空间推进系统的应用

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 41 期数: 2015年03期 页码: 15-20 栏目: 专论与综述 出版日期: 2015-06-30
Title:
Pneumopump technology and its application in space propulsion system
作者:
申智帅1;  2; 阮海军1;  2
1. 上海空间推进研究所，上海201112 2. 上海空间发动机工程技术研究中心，上海201112
Author(s):
SHEN Zhi-shuai1;  2;  RUAN Hai-jun1;  2
1. Shanghai Institute of Space Propulsion, Shanghai 201112, China 2. Shanghai Engineering Research Center of Space Engine, Shanghai 201112, China
关键词:
液体火箭发动机; 气动增压器技术; 研究进展; 关键技术; 空间推进
Keywords:
liquid propellant rocket engine;  pneumopump technology;  research evolution;  key technology;  space propulsion
分类号:
V434-34
文献标志码:
A
摘要:
液体火箭发动机用气动增压器技术在航天器推进系统中的应用，产生了一种全新的推进系统—气动增压式推进系统。介绍了气动增压器技术，分析了气动增压器技术应用于空间推进系统的优势和关键技术，并展望了应用前景。
Abstract:
The application of pneumopump technology for liquid rocket engine in space propulsion system has forced an implementation of a brand new propellant supply mode, that is, pneumopump space propulsion system, which is a great innovation in propellant supply system for liquid rocket. Pneumopump technology is introduced in this paper. The key technologies and advantages of pneumopump technology are analysed. The potential applications of pneumopump technology in space propulsion system are discussed.

参考文献/References:

[1]王新月. 气体动力学基础[M]. 西安: 西北工业大学出版社, 2010.
[2]YUZHNOYE S D O. Liquid rocket engine RD-860 [EB/ OL]. [2005-11-23]. http://www.yuzhnoye.com/index.
[3]SHNYAKIN V, PEREVERZEW V, SHUL'GA V, et al. Possible ways of increasing RD869 engine performance [C]// Proceedings of The 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. Bremen, Germany: IAF, 2003: 110-120.
[4]SHNYAKIN V, PEREVERZEW V, KONOKH V, et al. Pneumopump-fed liquid rocket engine [C]// Proceedings of The 55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. Vancouver, Canada: IAF, 2004: 104-110.

[5]SHNYAKIN V, SHUL'GA V, KONOKH V, et al. Propulsion system of DENPR LV fourth stage ground development results[C]// Proceedings of The 56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law. Fukuoka, Japan: IAF, 2005: 104-115.

[6]朱宁昌. 液体火箭发动机设计(上册) [M]. 北京: 宇航出版社, 1994.
[7]刘国球. 液体火箭发动机原理[M]. 北京: 宇航出版社, 1993.
[8]龙乐豪. 总体设计(上册)[M]. 北京: 宇航出版社, 1991.

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备注/Memo

收稿日期：2014-12-15；修回日期：2015-02-23 基金项目：上海市科学技术委员会资助课题(13DZ2250600) 作者简介：申智帅（1989—），男，硕士研究生，研究领域为航空宇航推进理论与工程

更新日期/Last Update: 1900-01-01