Firstly, according to the traits of the variablethrustengine, the hardware of the control system is designed.
首先结合变推力发动机的特点设计了数字控制器的硬件电路。
2
Flow in injector passages of a variablethrust liquid propellant rocket engine was studied.
本文对变推力液体火箭发动机喷注器通道内介质流动进行求解。
3
On the development process of the variablethrust rocket engine combustion vibra ions are encountered in the low working conditions, we solved this problem finely by lateral baffle.