| 内支撑式串联双星分离技术 |
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| 引用本文： | 范瑞祥,唐军刚,雷凯.内支撑式串联双星分离技术[J].导弹与航天运载技术,2012(4):1-4. |
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| 作者姓名： | 范瑞祥 唐军刚 雷凯 |
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| 作者单位： | 北京宇航系统工程研究所,北京,100076 |
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| 摘 要： | 内支撑式串联双星分离方案是国际主流运载火箭发射双星的优选方案。以CZ-2C/SMA火箭一箭双星发射环境A、B卫星方案为研究对象,介绍内支撑式结构布局、分离系统及典型分离时序,分析了双星分离的近场和远场关系。结果表明,该内支撑式串联双星分离方案合理、可行、安全性好。
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| 关 键 词： | 运载火箭 双星发射 内支撑 分离 上面级 |
Separation Technology of Dual Satellite for Internal Carrying Layout |
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| Fan Ruixiang
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Tang Jungang
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Lei Kai.Separation Technology of Dual Satellite for Internal Carrying Layout[J].Missiles and Space Vehicles,2012(4):1-4. |
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| Authors: | Fan Ruixiang Tang Jungang Lei Kai |
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| Affiliation: | (Beijing Institute of Astronautical Systems Engineering,Beijing,100076) |
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| Abstract: | The separation scheme of dual satellite for internal carrying layout is priority of the international mainstream vehicle.The dual satellite launch of CZ-2C/SMA,is studied and some issues related to the separation technique are introduced,including general layout scheme,separation system and the sequence of separation and the relations of near field and far field of the dual satellite separation is analyzed.The results indicate that this separation scheme is of reason,feasibility and safety. |
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| Keywords: | Launch vehicle Dual satellite launch Internal carrying Separation Upper stage |
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