|Table of Contents|

Pneumopump technology and its application in space propulsion system(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2015年03期
Page:
15-20
Research Field:
专论与综述
Publishing date:

Info

Title:
Pneumopump technology and its application in space propulsion system
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
Keywords:
liquid propellant rocket engine;  pneumopump technology;  research evolution;  key technology;  space propulsion
PACS:
V434-34
DOI:
-
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.

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.

Memo

Memo:
-
Last Update: 1900-01-01