The effect of the blocked spouts on the performance of an attitude control rocket 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。
This paper presents the critical design, researching method and procedure of acquisition system for valve current signal of liquid attitude control rocket 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。
The practical applications of this control system to the hypergolic bipropellant attitude control rocket 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。
In the instantaneous thrust measurement of an attitude control solid rocket motor, dynamic characteristic of thrust measurement system affects the accuracy of thrust measurement.
在姿控发动机的瞬态推力测量中，推力测量系统的动态特性是影响推力准确测量的一个至关重要的因素。
Carrying out launching attitude control is to increase the high concentration of rocket.
实施舰载多管火箭武器系统发射姿态控制的目的，是提高火箭发射的精度。
Carrying out launching attitude control is to increase the high concentration of rocket.
实施舰载多管火箭武器系统发射姿态控制的目的，是提高火箭发射的精度。
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