| 火星探测器减速着陆技术特点 |
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| 引用本文： | 荣伟,陈国良. 火星探测器减速着陆技术特点[J]. 航天返回与遥感, 2010, 31(4): 1-6 |
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| 作者姓名： | 荣伟 陈国良 |
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| 作者单位： | 北京空间机电研究所,北京,100076;北京空间机电研究所,北京,100076 |
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| 基金项目： | 中国空间技术研究院自主研发课题 |
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| 摘 要： | 针对火星上的稀薄大气环境和火星探测器的着陆要求,对火星探测器减速着陆技术进行了系统的分析,探讨了火星探测器减速着陆系统、气动外形、降落伞和着陆缓冲等相关环节的技术特点,为未来火星探测器减速着陆系统的设计提供参考。
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| 关 键 词： | 着陆技术 降落伞 火星探测器 |
The Characters of Deceleration and Landing Technology on Mars Explorer |
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| Rong Wei,Chen Guoliang. The Characters of Deceleration and Landing Technology on Mars Explorer[J]. Spacecraft Recovery & Remote Sensing, 2010, 31(4): 1-6 |
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| Authors: | Rong Wei Chen Guoliang |
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| Affiliation: | Rong Wei Chen Guoliang (Beijing Institute of Space Mechanics ＆ Electricity, Beijing, 100076, China) |
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| Abstract: | According to the Martian rare atmosphere environment and the landing requirements of Mars explorer, the deceleration and landing technologies on Mars explorer are analyzed in this paper. The technical characters of related parts, such as Mars explorer deceleration and landing system, aerodynamic configuration, parachute and landing cushion, are discussed. The results can provide some references for the design of Mars explorer deceleration of landing system in the future. |
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| Keywords: | Landing technology Parachute Mars explorer |
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