«Previous Article|Table of Contents|Next Article»

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

Issue:

2017年06期

Page:

38-43

Research Field:

研究与设计

Publishing date:

Info

Title:

Experimental study on pneumatic pressurization space propulsion system and its correlation technology

Author(s):

LIU Feng¹;  2;  SHEN Zhishuai¹;  2;  WANG Bo¹;  2;  CAO Wei¹;  2;  CHEN Jian¹;  2

1. Shanghai Institute of Space Propulsion, Shanghai 201112, China;2.Shanghai Engineering Research Center of Space Engine, Shanghai 201112, China

Keywords:

pneumatic pressurization;  liquid rocket engine;  propulsion system;  ground test

PACS:

V430-34

DOI:

-

Abstract:

The scheme and composition of the pneumatic pressurization space propulsion system are introduced. Experimental study on the new pneumatic pressurization liquid rocket engine technology is carried out. The test results and system performance related to the pneumatic pressurization space propulsion are analyzed emphatically. The results show that the pneumatic pressurization space propulsion system has the advantages of multiple start and high chamber pressure. The correlation technology was verified.

References:

[1] 申智帅, 阮海军. 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(3): 15-20.
SHEN Zhishuai, RUAN Haijun.Pneumopump technology and its applications in space propulsion system [J]. Journal of rocket propulsion, 2015, 41(3): 15-20.
[2] 朱明善, 刘颖, 林兆庄, 等. 工程热力学[M]. 北京:清华大学出版社, 2008.
[3] 申智帅, 陈剑, 刘锋. 提高增压气温度对气动增压系统的影响分析[C]//中国航天第三专业信息网第三十六届学术交流会会议论文集. 银川:[出版者不详], 2015: 79-84.
[4] 申智帅, 刘锋, 魏彦祥. 气体性质对气动增压器性能的影响[J]. 火箭推进, 2014, 40(4): 50-54.
SHEN Zhishuai, LIU Feng, WEI Yanxiang.Influences of gas properties on pneumopump performance[J]. Journal of rocket propulsion, 2014, 40(4): 50-54.
[5] 郭霄峰. 液体火箭发动机试验[M]. 北京: 中国宇航出版社, 2009.
[6] 龙乐豪. 总体设计(上册)[M]. 北京: 宇航出版社, 1991.
[7] 王新月. 气体动力学基础[M]. 西安: 西北工业大学出版社, 2010.
[8] 朱宁昌. 液体火箭发动机设计(上册)[M]. 北京: 宇航出版社, 1994.

Memo

Memo:

-

Common functions

Last Update: 1900-01-01