| 内装式机载发射运载火箭分离方案分析 |
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| 引用本文： | 康志宇,丁国锋,赵育善.内装式机载发射运载火箭分离方案分析[J].飞行力学,2005,23(1):65-67. |
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| 作者姓名： | 康志宇 丁国锋 赵育善 |
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| 作者单位： | 1. 西北工业大学,航天工程学院,陕西,西安,710072
2. 北京航空航天大学,宇航学院,北京,100083 |
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| 摘 要： | 针对一种内装式投放发射方案，建立了机载发射运载火箭分离过程的数学模型。本发射方案尢需对运载火箭进行改动。数值仿真结果表明．火箭在点火时有较好的姿态，适用于发射现有的中、小型运载火箭。
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| 关 键 词： | 空中发射 空中分离 运载火箭 |
| 文章编号： | 1002-0853(2005)01-0065-03 |
| 修稿时间： | 2004年2月4日 |
A Model of Launch Vehicles Departing from Loading-Aeroplane |
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| KANG Zhi-yu,Ding Guo-feng,ZHAO Yu-shan.A Model of Launch Vehicles Departing from Loading-Aeroplane[J].Flight Dynamics,2005,23(1):65-67. |
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| Authors: | KANG Zhi-yu Ding Guo-feng ZHAO Yu-shan |
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| Abstract: | With respect to the store-in-body rocket launching, a mathematical model for launch vehicle's department process when launching from a loading-aeroplane is established. The numberical simulation shows that the launch vehicle without any modification can be launched with a perfect attitude in launching, and the scheme can be used to launch all the used middle and small launch vehicles. |
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| Keywords: | air launch air-separation launch vehicle |
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