| 微型高压电磁阀的设计及应用 |
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| 引用本文： | 林涛,武葱茏,孙守黑.微型高压电磁阀的设计及应用[J].航天控制,2004,22(5):93-96. |
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| 作者姓名： | 林涛 武葱茏 孙守黑 |
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| 作者单位： | 北京控制工程研究所,北京,100080;北京控制工程研究所,北京,100080;北京控制工程研究所,北京,100080 |
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| 摘 要： | 要保持在国际卫星市场中强有力的竞争力 ,必须大力开展星上推进系统部件小型化的研制工作。本文详细介绍了微型高压电磁阀的工作原理、设计要点、结构形式、性能特性以及应用方向
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| 关 键 词： | 微小卫星 微型高压电磁阀 推进系统 |
| 文章编号： | 1006-3242(2004)05-0093-04 |
| 修稿时间： | 2004年5月30日 |
Design and Application of Micro High Pressure Solenoid Valve |
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| Lin Tao Wu Conglong Sun Shouhei Beijing Institute of Control Engineering,Beijing.Design and Application of Micro High Pressure Solenoid Valve[J].Aerospace Control,2004,22(5):93-96. |
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| Authors: | Lin Tao Wu Conglong Sun Shouhei Beijing Institute of Control Engineering Beijing |
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| Institution: | Lin Tao Wu Conglong Sun Shouhei Beijing Institute of Control Engineering,Beijing 100080 |
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| Abstract: | To keep the strong competition in the market of international satellite, it is necessary to develop the miniaturized assemblies for propulsion systems. The operating principle, design concept, configuration, performance and the future application direction of micro high pressure solenoid valve are presented in this paper. |
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| Keywords: | Subject terms Microsatellite Micro high pressure solenoid valve Propulsion system |
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