电火箭发动机是一种新型的空间推进装置。
Electrical rocket engine is a new type of 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。
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.
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