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某舱外载荷设备热控设计及验证

齐晓巧 朱清淋 杨雷 乔志宏

空间科学学报2026,Vol.46Issue(2):392-402,11.
空间科学学报2026,Vol.46Issue(2):392-402,11.DOI:10.11728/cjss2026.02.2025-0050

某舱外载荷设备热控设计及验证

Thermal Control Design and Verification of Extravehicular Load Equipment

齐晓巧 1朱清淋 2杨雷 3乔志宏2

作者信息

  • 1. 北华航天工业学院机电工程学院 廊坊 065000
  • 2. 中国科学院空间应用工程与技术中心 北京 100094
  • 3. 北京中科宇航技术有限公司创新中心 北京 100176
  • 折叠

摘要

Abstract

In order to solve the problem of frequency stability and transmission accuracy decrease caused by temperature fluctuation during on-orbit operation of an extravehicular load equipment,a high-ly efficient thermal control scheme is proposed which bases on passive thermal control as the main ap-proach and active thermal control as the auxiliary method.The scheme employs a single-phase liquid cold plate as the main heat dissipation surface,and 10-unit multi-layer insulation components for com-prehensive encapsulation.High thermal conductivity materials are utilized to achieve efficient heat con-duction.Simultaneously,heating sheets and TEC semiconductor ceramic sheets are used for precise tem-perature control.Through finite element simulation analysis of temperature distribution under both high and low temperature conditions and optimization design,the temperature variation of key components is controlled within±0.5 K.The ground constant-temperature thermal balance experiment and the in-or-bit data results indicate that this scheme effectively suppresses the interference of temperature fluctua-tions on the load equipment,significantly improves the overall temperature uniformity of the equipment.It enables photodiodes and other sensitive devices to operate within the optimal temperature range(25-50℃).The temperature change rate of temperature-sensitive devices on the extravehicular load equip-ment is better than 0.1 K·min-1,meeting the on-orbit stability requirements of high-precision time-fre-quency transmission systems.It can provide an important reference for the thermal control design of similar space load equipment.

关键词

舱外/载荷设备/热控设计/有限元/热平衡实验

Key words

Extravehicular/Load equipment/Thermal control design/Finite element/Thermal balance experiment

分类

航空航天

引用本文复制引用

齐晓巧,朱清淋,杨雷,乔志宏..某舱外载荷设备热控设计及验证[J].空间科学学报,2026,46(2):392-402,11.

基金项目

中国载人航天工程空间站载荷研制项目(T0182411PN),博士科研启动基金项目(BKY-2022-11)和廊坊市科技支撑计划项目(2022011018,2022011024)共同资助 (T0182411PN)

空间科学学报

0254-6124

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