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[1]姜文龙,杨成虎,林庆国.高性能卫星用490 N轨控发动机研究进展[J].火箭推进,2011,37(06):9-13.
　JIANG Wen-long,YANG Cheng-hu,LIN Qing-guo.Development of high performance 490 N apogee engine for satellites[J].Journal of Rocket Propulsion,2011,37(06):9-13.
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高性能卫星用490 N轨控发动机研究进展

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 37 期数: 2011年06期 页码: 9-13 栏目: 专论与综述 出版日期: 2011-12-15
Title:
Development of high performance 490 N apogee engine for satellites
文章编号:
1672-9374(2011)06-0009-05
作者:
姜文龙; 杨成虎; 林庆国
上海空间推进研究所，上海 200233
Author(s):
JIANG Wen-long;  YANG Cheng-hu;  LIN Qing-guo
Shanghai Institute of Space Propulsion, Shanghai 200233, China
关键词:
液体远地点发动机; 比冲性能; 进展
Keywords:
liquid apogee engine;  specific impulse;  progress
分类号:
V434-34
文献标志码:
A
摘要:
阐述了卫星用第三代高性能490 N轨控发动机的研究进展，主要介绍了发动机的设计概况、试验验证情况以及关键技术攻关情况。对后续研制工作提出了初步设想。
Abstract:
The progress of the third generation high performance 490 N apogee engine for satellites is elaborated in this paper. The engine design, hot firing test and the key technology research are described. At last the tentative plan for the follow-up development work is introduced.

参考文献/References:

[1]STECHMAN Carl, KRISTER David. Off-limit testing of the model R-4D 110LBF(490N) bipropellant rocket engine, AIAA2004-3694[R]. USA: AIAA, 2004.
[2]WU P K, WOLL P, STECHMAN Carl. Qualification testing of 2nd generation high performance apogee thruster, AIAA2001-3253[R]. USA: AIAA, 2001.
[3]STECHMAN Carl, WOLL Peter. A high performance liquid rocket engine for satellite main propulsion, AIAA2000-3161 [R]. USA: AIAA, 2000.
[4]SCHOENMAN L, ROSENBERG S D. Test experience，490N high performance[321 Sec Isp] engine, AIAA92-3800 [R]. USA: AIAA, 1992.
[5]张中光, 钟徐. “神舟”号载人飞船轨控发动机的研制[J].上海航天, 2004 (1): 2-9.
[6]HARDING J T, KAZAROFF J M, APPEL M A. Iridium-coated rhenium thrusters by CVD, TM-101309[R]. USA: NASA, 1988.

相似文献/References:

[1]周红玲,等.国内外卫星用液体远地点发动机发展综述[J].火箭推进,2011,37(05):1.
　ZHOU Hong-ling,JIANG Wen-long,et al.Development of liquid apogee engine for satellite at home and abroad[J].Journal of Rocket Propulsion,2011,37(06):1.
[2]银仁亮,周进,张中光,等.液体远地点发动机推力室工作过程数值仿真[J].火箭推进,2004,(04):6.
　Yin Renliang,Zhou Jin,Zhang Zhongguang.Numerical Simulation of Operation Process of Liquid Apogee Engine Thrust Chamber[J].Journal of Rocket Propulsion,2004,(06):6.

备注/Memo

收稿日期：2011-05-13；修回日期：2011-08-12
作者简介：姜文龙（1980—），男，高级工程师，研究领域为液体火箭发动机设计和制造

更新日期/Last Update: 1900-01-01