| 新舟60飞机起飞性能分析 |
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| 引用本文： | 王东,陈红英,郑孝雍,余江.新舟60飞机起飞性能分析[J].中国民航飞行学院学报,2011(5):36-39. |
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| 作者姓名： | 王东 陈红英 郑孝雍 余江 |
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| 作者单位： | 中国民航飞行学院,四川广汉,618307 |
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| 摘 要： | 从新舟60(MA60)的飞机飞行手册(AFM)和飞行机组操纵手册(FCOM)入手,分析了限制最大起飞重量的因素和起飞速度的选择方法,着重讨论了MA60最大起飞重量的限制因素,并以MA60从广汉至兰州的航线飞行为例分析了最大起飞重量和起飞速度的确定方法。
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| 关 键 词： | MA60 最大起飞重量 起飞速度 爬升梯度 |
Analysis on MA60 Aircraft Takeoff Performance |
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| Wang Dong Chen Hongying Zhen Xiaoyong Yu Jiang.Analysis on MA60 Aircraft Takeoff Performance[J].Journal of China Civil Aviation Flying College,2011(5):36-39. |
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| Authors: | Wang Dong Chen Hongying Zhen Xiaoyong Yu Jiang |
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| Institution: | Wang Dong Chen Hongying Zhen Xiaoyong Yu Jiang (Civil Aviation Flight University of China Guanghan 618307 Sichuan China) |
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| Abstract: | Based on MA60 Aircraft Flight Manual(AFM) and Flight Crew Operation Manual (FCOM),this paper analyses the limit factors of maximum takeoff weight and the ways of selecting takeoff velocity.In the case study of the typical flight route from Guanghan to Lanzhou the authors pinpoint the limit factors of maximum takeoff weight and the selection of takeoff velocity for MA60. |
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| Keywords: | MA60 Maximum takeoff weight Takeoff velocity Climb gradient |
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