| 火星探测器减速着陆技术分析 |
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| 引用本文： | 贾贺,荣伟.火星探测器减速着陆技术分析[J].航天返回与遥感,2010,31(3):6-14. |
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| 作者姓名： | 贾贺 荣伟 |
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| 作者单位： | 北京空间机电研究所,北京,100076 |
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| 基金项目： | 国家重大科技专项工程 |
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| 摘 要： | 火星的大气环境和地球差异较大,存在着许多未知的因素,火星探测的减速着陆同样充满了风险和挑战。文章通过对美国火星探测减速着陆的重点技术进行分析,并归纳总结了火星探测器减速着陆技术的发展趋势。
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| 关 键 词： | 火星探测器 减速着陆 缓冲技术 |
Mars Exploration Deceleration Landing Technology Analysis |
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| Jia He,Rong Wei.Mars Exploration Deceleration Landing Technology Analysis[J].Spacecraft Recovery & Remote Sensing,2010,31(3):6-14. |
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| Authors: | Jia He Rong Wei |
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| Institution: | Jia He Rong Wei(Beijing Institute of Space Mechanics ＆ Electricity,Beijing 100076,China) |
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| Abstract: | There are great differences between the atmosphere environment of Mars and Earth,the deceleration landing of Mars will be full of risks and challenges for the unknown factors of Mars atmosphere environment.Through analyzing the key Mars exploration deceleration landing techniques of USA,the trends of Mars explorer deceleration landing technology development are summarized. |
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| Keywords: | Mars explorer Deceleration landing Cushion technology |
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