摘要
某靶标巡航系统采用了小推力液体火箭发动机,该火箭发动机关系到整个靶标系统的可靠性。分析了该巡航系统小推力液体火箭发动机,设计了其地面试验系统,分析得到了系统搭建的关键参数,提出了贮箱自动稳压与系统测试方案,从而为试验系统应用提供了理论依据。
A target cruise system is powered by the low- thrust liquid rocket engine,and the rocket engine is related to the reliability of the whole target system. The ground test system is designed through analysis of low - thrust liquid rocket en- gine. The key parameters of the test system are obtained, the scheme of automatic pressure - regulating and system test is put forward,it provides a theoretical basis for the application of the test system.
出处
《现代机械》
2017年第3期54-57,共4页
Modern Machinery
基金
贵州省工业攻关项目(黔科合GZ字[2015]3028)
