takeoff weight

The results show that during the takeoff buffer phase, the Chinese long jump elites' horizontal velocity of center of body weight decreases, while their vertical velocity increases, both of which have a close relation;

结果表明，我国优秀男子跳远运动员起跳缓冲阶段，身体重心水平速度减小，并与垂直速度增加之间存在密切关系；

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The plane has a maximum takeoff weight of 53.5 tons, and is able to carry 50 people during a maritime search and rescue mission.

AG600最大起飞重量53.5吨，水上应急救援可以一次性救护50名人员。

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The task of the initial sizing is to find the primary parameters of aircraft, including the takeoff wing loading, thrust-to-weight ratio, takeoff weight, wing area, aspect ratio of wing, wing sweep, thickness and taper ratio to match the mission requirements.

其任务是找到能满足飞机性能要求的飞机主要参数。这些参数包括：起飞翼载、推重比、起飞重量、机翼面积、机翼翼载、机翼后掠角、机翼相对厚度和机翼梯形比等。

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AIRPORT ANALYSIS, A comprehensive set of takeoff weight limitations for a given airport runway, generally presented as a function of airport temperature, wind, and aircraft flap setting.

机场分析，一套针对给定的机场跑道的详细重量限制资料。通常与机场温度、风、和飞机襟翼位置成函数关系。

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By using this carpet plot, a designer can conveniently select the values of the wing loading and the thrust-to-weight ratio to minimize the takeoff weight, while still meeting the performance requirements.

通过地毯图，设计人员可以选取在满足飞机各个设计性能要求约束下使得飞机起飞重量最小的推重比和翼载的组合。

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The maximum takeoff weight based on the ability of the brakes to absorb a predetermined amount of energy during a rejected takeoff.

中断起飞过程中，取决于刹车吸收预定能量之能力的最大起飞重量。

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In the carpet plot module, the relation of the aircraft takeoff weight with the wing loading and thrust-to-weight ratio are displayed on the carpet plot, and various requirement boundaries are also plotted on the same plot.

在地毯图中，描述了飞机推重比和翼载与客机最大起飞重量之间的相互关系。同时依据界限线的绘制方法，也将客机各个设计性能要求绘制在同一张图上。

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The maximum takeoff and landing weight to be used for each type of aircraft;

各型航空器所使用的最大起飞重量和最大着陆重；

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Powered by four domestically designed WJ-6 turboprop engines, it has a maximum takeoff weight of 53.5 metric tons.

AG600由四台国产涡桨-6涡轮螺旋桨发动机提供动力，最大起飞重量达53.5吨。

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By searching and sorting out the data of existing WIG, the statistic relationship of takeoff weight and empty weight as well as other parameters are studied.

通过现有地效飞行器数据和资料的整理，研究其起飞重量与空机重量以及其他各项参数的统计关系。

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