李爽1,2, 江秀强1,2
CJA
收稿日期:2014-04-15
修回日期:2014-10-08
出版日期:2015-02-15
发布日期:2014-10-09
通讯作者:
李爽 Tel.: 025-84896039 E-mail: lishuang@nuaa.edu.cn
E-mail:lishuang@nuaa.edu.cn
作者简介:李爽 男,博士,教授。主要研究方向:航天器动力学与控制、深空探测和航天技术新概念。Tel:025-84896039 E-mail:lishuang@nuaa.edu.cn;江秀强 男,硕士研究生。主要研究方向:新型火星大气进入、下降与着陆的导航、制导与控制。Tel:025-84892805 E-mail:jiangxq@nuaa.edu.cn
基金资助:国家自然科学基金(61273051,60804057);国家"863"计划(2011AA7034057E,2012AA121601)
LI Shuang1,2, JIANG Xiuqiang1,2
Received:2014-04-15
Revised:2014-10-08
Online:2015-02-15
Published:2014-10-09
Supported by:National Natural Science Foundation of China (61273051, 60804057); National High-tech Research and Development Program of China (2011AA7034057E, 2012AA121601)
摘要：
随着火星着陆探测任务的不断推进,火星采样返回、载人登陆火星和火星基地等任务要求能将更大、更重的探测器着陆到火星表面,这就需要在火星大气进入阶段进行高效减速。基于以往成功的火星着陆探测任务,首先系统地回顾了火星进入段气动减速技术的发展历史;然后,结合火星进入过程的特点阐述了火星进入段减速设计的必要性及其面临的挑战;接着,系统地总结了充气式气动减速器、可展开式气动减速器和超声速反推减速器的系统构成和研究进展;最后,对这3种减速器技术的未来发展方向和亟待解决的关键问题进行了比较全面的分析和展望。
中图分类号:
李爽, 江秀强. 火星进入减速器技术综述与展望[J]. 航空学报, 2015, 36(2): 422-440.
LI Shuang, JIANG Xiuqiang. Review and prospect of decelerator technologies for Mars entry[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(2): 422-440.
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