Flow in injector passages of a variable thrust liquidpropellantrocketengine 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。
2
This paper presents the development of the liquidpropellantrocketengine technology from the viewpoint of combustion chamber pressure, thrust level and power cycle.
本文从燃烧室压力、系统工作循环方式以及最大推力三个方面叙述了世界各国液体火箭发动机的技术水平。
3
Firstly, the static and dynamic mathematic model of the LiquidPropellantRocketEngine of pressure-fed providing system was established in centralized parameter method.