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我国火星软着陆探测技术发展成就

孙泽洲 董捷 饶炜 贾阳 王闯 陈百超

航天器工程2024,Vol.33Issue(6):14-20,7.
航天器工程2024,Vol.33Issue(6):14-20,7.DOI:10.3969/j.issn.1673-8748.2024.06.002

我国火星软着陆探测技术发展成就

Development Achievements of China's Mars Soft-landing Exploration Technology

孙泽洲 1董捷 1饶炜 1贾阳 1王闯 1陈百超1

作者信息

  • 1. 北京空间飞行器总体设计部,北京 100094
  • 折叠

摘要

Abstract

The main characteristics and difficulties of the Mars soft-landing exploration mission are analyzed in this paper.Based on the outline plan of China's first Mars soft-landing probe,it in-troduces the overall design of the probe and the development and innovation of 9 key technology(guidance,navigation and control,lightweight thermal protection,high temperature and large load bearing structure,large supersonic low dynamic pressure parachute,medium chamber pres-sure variable thrust bi-component space propulsion,Mars environment simulation and verifica-tion,etc.),then the main achievements are summarized.

关键词

火星探测/软着陆/总体设计

Key words

Mars exploration/soft-landing/overall design

分类

航空航天

引用本文复制引用

孙泽洲,董捷,饶炜,贾阳,王闯,陈百超..我国火星软着陆探测技术发展成就[J].航天器工程,2024,33(6):14-20,7.

航天器工程

OA北大核心CSTPCD

1673-8748

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