火箭推进2012，Vol.38Issue(5)：18-23,6.
卫星单元肼推进系统安全陛设计与实现
Safety design and realization of hydrazine monopropellant propulsion system for satellites
摘要
Abstract
The safety design philosophies for the existing hydrazine monopropellant propulsion systems in satellites are introduced and analyzed in the aspects of power distribution protection, fault isolation, safety margin design, etc. Implementation and validation both on ground and in orbit are also described. Several suggestions on safety design are proposed through analysis and summarization.关键词
卫星/单元肼推进系统/安全性设计Key words
satellite/hydrazine monopropellant propulsion system/safety design分类
航空航天引用本文复制引用
何永英..卫星单元肼推进系统安全陛设计与实现[J].火箭推进,2012,38(5):18-23,6.基金项目
中国航天科技集团公司支撑项目 （）
