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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 uses a small thrust liquid rocket engine, the rocket engine related to the reliability of the entire target system. The small thrust liquid propellant rocket engine of the cruise system is analyzed and the ground test system is designed. The key parameters of the system are analyzed and the automatic tank pressure regulator and system test scheme are put forward, which provides a theoretical basis for the application of the test system.