空间站专栏

空间站的碎片防护设计与实践

  • 闫军 ,
  • 郑世贵 ,
  • 于伟 ,
  • 宫伟伟
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  • 北京空间飞行器总体设计部,北京 100094
闫军(1970—),博士,研究员,主要从事航天器防护设计和航天器动力学领域工作,参与了天宫一号和空间站的防护设计任务。通信地址:北京市5142信箱368分箱(100094)电子邮箱:jun.yan@263.net

网络出版日期: 2023-12-12

Space Debris Protection Design for the Space Station

  • YAN Jun ,
  • ZHENG Shi-gui ,
  • YU Wei ,
  • GONG Wei-wei
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  • Beijing Institute of Spacecraft System Engineering,Beijing 100094,China

Online published: 2023-12-12

摘要

总重量可能达到60~70t的空间站将是中国发射入轨的最大航天器,如何避免其遭受微流星体和空间碎片的威胁成为至关重要的问题。本文对我国空间站的空间碎片防护设计过程进行了回顾,包括风险评估、防护结构研制及防护设计等。经防护设计后的空间站PNP值从未加防护的0.0000提高到防护后的0.9397。

本文引用格式

闫军 , 郑世贵 , 于伟 , 宫伟伟 . 空间站的碎片防护设计与实践[J]. 空间科学与试验学报, 2021 , 21(2) : 1 -9 . DOI: 10.19963/j.cnki.2096-4099.2021.02.001

Abstract

The Chinese space station is expected to have a mass between 60-70 tons,and will be the largest spacecraft that China has ever launched into orbit in the history.How to shield the station from risks of micro-meteoroid and space debris is a very important technology.The paper summarizes the development history of the shielding technology for Chinese space station,including the risk assessment,shielding structure development and optimization.The PNP of the Chinese space station rises from 0.000 to 0.9397 after shielding design.

参考文献

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