| Ivar asteroid rendezvous mission system scenario and trajectory design |
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| 作者姓名： | 崔平远 李立涛 崔祜涛 栾恩杰 吴伟仁 田玉龙 |
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| 作者单位： | Deep Space Exploration Research Center，Harbin Institute of Technology，Harbin 150001，China，Deep Space Exploration Research Center，Harbin Institute of Technology，Harbin 150001，China，Deep Space Exploration Research Center，Harbin Institute of Technology，Harbin 150001，China，China National Space Administration，Beijing 100037，China，China National Space Administration，Beijing 100037，China，China National Space Administration，Beijing 100037，China |
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| 摘 要： | The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to 2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed, and the transfer trajectory is designed using △VEGA technology for the asteroid rendezvous. The design results satisfied the energy requirements for small explorers.
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Ivar asteroid rendezvous mission system scenario and trajectory design |
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| CUI Ping-yuan.Ivar asteroid rendezvous mission system scenario and trajectory design[J].Journal of Harbin Institute of Technology,2003,10(3). |
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| Authors: | CUI Ping-yuan |
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| Affiliation: | 1. Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China
2. China National Space Administration, Beijing 100037, China |
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| Abstract: | The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed,and the transfer trajectory is designed using △VEGA technology for the asteroid rendezvous. The design resultssatisfied the energy requirements for small explorers. |
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| Keywords: | trajectory design rendezvous spacecraft system design asteroid exploration |
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