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[1]刘锋,申智帅,王波,等.气动增压空间推进系统及相关技术试验研究[J].火箭推进,2017,43(06):38-43.
　LIU Feng,SHEN Zhishuai,et al.Experimental study on pneumatic pressurization space propulsion system and its correlation technology[J].Journal of Rocket Propulsion,2017,43(06):38-43.
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气动增压空间推进系统及相关技术试验研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 43 期数: 2017年06期 页码: 38-43 栏目: 研究与设计 出版日期: 2017-12-30
Title:
Experimental study on pneumatic pressurization space propulsion system and its correlation technology
文章编号:
1672-9374(2017)06-0038-06
作者:
刘锋1; 2; 申智帅1; 2; 王波1; 2; 曹伟1; 2; 陈剑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):
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
关键词:
气动增压器;  液体火箭发动机;  推进系统;  地面试车
Keywords:
pneumatic pressurization;  liquid rocket engine;  propulsion system;  ground test
分类号:
V430-34
文献标志码:
A
摘要:
简要介绍了气动增压空间推进系统方案及组成,开展了基于气动增压原理的新型发动机技术试验研究,重点分析了气动增压空间推进相关技术试验结果和系统性能。结果表明,气动增压空间推进系统同时具备多次起动和高室压的优点,相关技术得到了验证。
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.

参考文献/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.
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[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.
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备注/Memo

收稿日期:2016-08-05
基金项目:上海市科学技术委员会资助项目(13DZ2250600)
作者简介: 刘锋(1971—),男,研究员,研究领域为液体火箭发动机系统设计

更新日期/Last Update: 1900-01-01