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我国深空探测器热控技术发展

陈阳 张有为 宁献文 张红星 张冰强 王录 吕巍 蒋凡 陈庆 苗建印 陈建新 向艳超 张栋 赵亮 邵兴国 刘自军

航天器工程2024,Vol.33Issue(6):82-91,10.
航天器工程2024,Vol.33Issue(6):82-91,10.DOI:10.3969/j.issn.1673-8748.2024.06.010

我国深空探测器热控技术发展

Development of Thermal Control Technology for Deep Space Exploration Spacecraft in China

陈阳 1张有为 1宁献文 1张红星 1张冰强 1王录 1吕巍 1蒋凡 1陈庆 1苗建印 1陈建新 1向艳超 1张栋 1赵亮 1邵兴国 1刘自军1

作者信息

  • 1. 北京空间飞行器总体设计部 航天器热控技术全国重点实验室,北京 100094
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摘要

Abstract

Spacecraft thermal control technology has been crucial in securing the success of a series of deep space exploration missions,including China's Lunar Exploration Program(CLEP)Chang'e-1 to Chang'e-6 and its Mars exploration mission Tianwan-1.China has accumulated ad-vanced design experiences and overcame a series of significant technical challenges such as high-temperature heat dissipation and low-temperature survival in low-gravity and medium-vacuum en-vironments.This paper provides a comprehensive review of the system designs,technological in-novation,product development,and engineering practice of thermal control for deep space explo-ration spacecraft over the 20-year span of CLEP.Coverage includes the development of thermal environment models for planets,active and passive thermal control technologies,and thermal testing technologies,with detailed explanations of their respective technological characteristic sprinciple and application performance.Furthermore,based on the developmental needs and challenge for China's upcoming deep space exploration missions,some recommendations are pro-vided for advancing thermal control technologies tailored to future deep space exploration spacecraft.

关键词

深空探测/热控技术/进展/展望

Key words

deep space exploration/thermal control technology/development/prospect

分类

航空航天

引用本文复制引用

陈阳,张有为,宁献文,张红星,张冰强,王录,吕巍,蒋凡,陈庆,苗建印,陈建新,向艳超,张栋,赵亮,邵兴国,刘自军..我国深空探测器热控技术发展[J].航天器工程,2024,33(6):82-91,10.

航天器工程

OA北大核心CSTPCD

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