|Table of Contents|

Developing progress of liquid bipropellant orbit control engine for high orbit satellite(PDF)

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

Issue:
2018年01期
Page:
1-7
Research Field:
专论与综述
Publishing date:

Info

Title:
Developing progress of liquid bipropellant orbit control engine for high orbit satellite
Author(s):
ZHAO Ting;  CHEN Xiachao; YANG Chenghu;  YAO Feng;  LIU Changguo
Shanghai Institute of Space Propulsion, Shanghai 201112, China
Keywords:
high orbit satellite;  orbit control engine;  specific impulse performance;  research progress
PACS:
V439.7-34
DOI:
-
Abstract:
The development and status quo of liquid orbit control engine for high orbit satellite is summarized.The development course(the first generation, the second generation to the third generation)of the 490 N orbit control engine is introduced briefly in this paper.The development status, technical solution and test result of 750 N high-performance orbit control engine are described.Development experience of orbit control engine for satellite in China is summarized.According to current technical state of China, the specific impulse of the 750 N orbit control engine with niobium alloy combustor can reach more than 321 s, and its working life can meet the requirements of 25 000 s.Compared with the high-performance liquid orbit control engines in foreign countries, the 750 N engine used for high orbit satellite has reached the international advanced level.

References:

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[7] 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(6):9-13.
JIANG Wenlong, YANG Chenghu, LIN Qingguo. Development of high performance 490 N apogee engine for satellites [J]. Journal of rocket propulsion, 2011,37(6): 9-13.
[8] 杨成虎,林庆国,刘昌国.高性能液体远地点发动机技术发展[J].火箭推进,2013,39(4):1-7.
YANG Chenghu, LIN QINGguo, LIU Changguo. Technology development of high-performance liquid apogee engine [J]. Journal of rocket propulsion, 2013, 39(4): 1-7.

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Last Update: 1900-01-01