Electrical rocket engine is a new type of space propulsion system.
电火箭发动机是一种新型的空间推进装置。
Hydrazine decomposition thruster with canted nozzle is being more and more utilized in space propulsion system.
折角喷管肼分解发动机在空间推进系统正得到越来越多的应用。
The general integral equations are derived for liquid and gas components of space propulsion systems with liquid propellant rocket engine.
针对采用液体推进剂火箭发动机的空间推进系统,推导了系统液路和气路的通用积分形式方程。
应用推荐