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。
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.
出处
《航天控制》
CSCD
北大核心
2004年第5期93-96,共4页
Aerospace Control
关键词
微小卫星
微型高压电磁阀
推进系统
Subject terms Microsatellite Micro high pressure solenoid valve Propulsion system
