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Thermal Control Design and Verification of Extravehicular Load Equipment
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Xiaoqiao QI1, Qinglin ZHU2, Lei YANG3, Zhihong QIAO2
Chinese Journal of Space Science | 2026, 46(2) : 392 - 402
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Chinese Journal of Space Science | 2026, 46(2): 392-402
Research Article
Thermal Control Design and Verification of Extravehicular Load Equipment
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Xiaoqiao QI1, Qinglin ZHU2, Lei YANG3, Zhihong QIAO2
Affiliations
  • 1School of Mechanical and Electrical Engineering, North China Institute of Aerospace Engineering, Langfang 065000
  • 2Institute of Space Application Engineering and Technology, Chinese Academy of Sciences, Beijing 100094
  • 3InnovCenter, Beijing Zhongke Aerospace Technology Co., Ltd., Beijing 100176
Published: 2026-03-15 doi: 10.11728/cjss2026.02.2025-0050
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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 highly efficient thermal control scheme is proposed which bases on passive thermal control as the main approach 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 comprehensive encapsulation. High thermal conductivity materials are utilized to achieve efficient heat conduction. Simultaneously, heating sheets and TEC semiconductor ceramic sheets are used for precise temperature 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-orbit data results indicate that this scheme effectively suppresses the interference of temperature fluctuations 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°C). The temperature change rate of temperature-sensitive devices on the extravehicular load equipment is better than 0.1 K·min–1, meeting the on-orbit stability requirements of high-precision time-frequency transmission systems. It can provide an important reference for the thermal control design of similar space load equipment.

Extravehicular  /  Load equipment  /  Thermal control design  /  Finite element  /  Thermal balance experiment
Xiaoqiao QI, Qinglin ZHU, Lei YANG, Zhihong QIAO. Thermal Control Design and Verification of Extravehicular Load Equipment[J]. Chinese Journal of Space Science, 2026 , 46 (2) : 392 -402 . DOI: 10.11728/cjss2026.02.2025-0050
Year 2026 volume 46 Issue 2
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Article Info
doi: 10.11728/cjss2026.02.2025-0050
  • Receive Date:2025-04-03
  • Online Date:2026-07-08
  • Published:2026-03-15
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History
  • Received:2025-04-03
  • Revised:2026-01-12
Affiliations
    1School of Mechanical and Electrical Engineering, North China Institute of Aerospace Engineering, Langfang 065000
    2Institute of Space Application Engineering and Technology, Chinese Academy of Sciences, Beijing 100094
    3InnovCenter, Beijing Zhongke Aerospace Technology Co., Ltd., Beijing 100176
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小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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