| 火箭内装式机载发射运载能力分析 |
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| 引用本文： | 丁国锋,赵育善.火箭内装式机载发射运载能力分析[J].飞行力学,2006,24(2):40-42. |
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| 作者姓名： | 丁国锋 赵育善 |
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| 作者单位： | 北京航空航天大学,宇航学院,北京,100083 |
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| 摘 要： | 针对内装式机载发射运载火箭的分离方案,结合分离条件及某型号运载火箭,设计了火箭分离后的发射轨道,并研究了火箭的控制规律。分析和计算表明,所设计的发射轨道可满足卫星发射需求,所采取的控制规律切实可行,与地面发射相比,可大幅度提高运载火箭的发射能力。
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| 关 键 词： | 机载发射 运载火箭 运载能力 |
| 文章编号： | 1002-0853(2006)02-0040-03 |
| 收稿时间： | 2005-03-29 |
| 修稿时间： | 2006-01-06 |
Analysis on Power of Air-Borne Inside Launch Vehicles |
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| DING Guo-feng,ZHAO Yu-shan.Analysis on Power of Air-Borne Inside Launch Vehicles[J].Flight Dynamics,2006,24(2):40-42. |
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| Authors: | DING Guo-feng ZHAO Yu-shan |
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| Institution: | School of Astronautics ,Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | With respect to the departing model of air-borne launch vehicles,a launch vehicle's trajectory is designed with departing condition and certain launch vehicle,the research on its controlling method is also done.The analysis and result indicate that its trajectory could fit the bill and the controlling method is effective.Compared with the model of launching from ground,the air-borne launch vehicle can improve its power by great extent. |
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| Keywords: | air-borne launch vehicle launch power |
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