假设温度是由飞机实际起飞质量确定的相当的大气温度。
Assumed temperature is the equivalent ambient air temperature determined by the actual takeoff mass of an aircraft.
在给定有效载荷、最高射高的条件下，选取动力系统的设计参数使火箭的起飞质量最小。
Under the conditions of the given payload and the highest launching height, the design parameters of the propulsion system are selected to minimize takeoff mass of the rocket.
最后讨论了飞机的起飞质量，发动机推力、起飞迎角、襟翼偏角和甲板风航迹等对弹射起飞性能的影响。
Finally, a brief discussion is present about the influence of the airplane gross weight, the thrust, the maximum Angle of attack, the flap Angle and the wind over the deck on...
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