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。
Hydrazine decomposition thruster with canted nozzle is being more and more utilized in space propulsion system.
单组元肼分解发动机的热控制与热分析是空间推进系统重要组成部分。
Thermal control of monopropellant catalytic decomposition hydrazine engines in important portion of space propulsive system.
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。
The general integral equations are derived for liquid and gas components of space propulsion systems with liquid propellant rocket engine.
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