| 一种高可靠长寿命的推进系统 |
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| 引用本文： | 蒋光林.一种高可靠长寿命的推进系统[J].推进技术,1994,15(4):27-33. |
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| 作者姓名： | 蒋光林 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 介绍单元肼为推进剂的卫星推进系统，该系统已成功用于我国地球同步轨道通信卫星，高可靠，长寿命。叙述了系统及各部件的主要性能，关键部件的特性与可靠性试验，材料相容性试验，微粒控制及系统热试车。根据多年的飞行试验及地验对系统进行了可靠性计算。
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| 关 键 词： | 肼发动机 单元推进剂 可靠性 卫星 |
A LONG-LIFE HIGH-RELIABILITY PROPULSION SYSTEM |
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| Jiang Guanglin.A LONG-LIFE HIGH-RELIABILITY PROPULSION SYSTEM[J].Journal of Propulsion Technology,1994,15(4):27-33. |
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| Authors: | Jiang Guanglin |
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| Institution: | Beijing Institute of Control Engineering, Beijing,100080 |
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| Abstract: | A monopropellant hydrazine propulsion system for satellite, which has been successfully used to launch the China geostationary communication satellite, is presented. The propulsion system is long-life and high-reliability one. The preformance of this system and its components, the characteristic of critical components and reliability test, the compatibility test of materials, the control of microparticles and whole system firing test are also discussed. The reliability calculationhas been carried out based on the data in flight and ground tests. |
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| Keywords: | Hydrazine engine Monopropellant High reliabilty Service life Satellite attitude control |
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