The practical applications of this control system to the hypergolic bipropellant attitudecontrolrocket engines at 30kg and 100kg thrust levels respectively are stated.
说明了该控制系统在30公斤级与100公斤级的双组元燃料变推力姿控火箭发动机中的具体应用情况。
2
This paper presents the critical design, researching method and procedure of acquisition system for valve current signal of liquid attitudecontrolrocket 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
In the instantaneous thrust measurement of an attitudecontrol solid rocket motor, dynamic characteristic of thrust measurement system affects the accuracy of thrust measurement.