火箭推进2012，Vol.38Issue(1)：12-16,26,6.
新型活塞泵增压轨／姿控发动机系统方案研究
Scheme study on divert and attitude control engines with piston pump pressurized system
摘要
Abstract
The development of foreign piston pump pressurized systems for the divert and attitude control engines is narrated. A new scheme of divert and attitude control engine with a piston pump pressurized system is brought out. The system characteristics are introduced and the key technologies are analyzed. The scheme of a new piston pump pressurized system for divert and attitude control engines is studied. The design technologies of main components have been mastered. The simulation characteristics of the piston pump pressurized system were obtained.关键词
活塞泵/增压系统/轨／姿控发动机Key words
piston pump/pressurized system/divert and attitude control engine分类
航空航天引用本文复制引用
李淑艳,肖明杰,李晓瑾,郑小鹏,董万峰..新型活塞泵增压轨／姿控发动机系统方案研究[J].火箭推进,2012,38(1):12-16,26,6.基金项目
总装备部预研项目 （）
