The effect of the blocked spouts on the performance of an attitude controlrocket motor was analyzed by using numerical simulation and test.
通过数值模拟和试验研究，分析了喷口遮挡对姿控火箭发动机性能的影响。
2
This paper presents the critical design, researching method and procedure of acquisition system for valve current signal of liquid attitude controlrocket engine.
介绍了液体火箭姿控发动机阀门电流信号采集系统的设计要点、研制方法与主要开发过程。
3
The practical applications of this control system to the hypergolic bipropellant attitude controlrocket engines at 30kg and 100kg thrust levels respectively are stated.