AEROSPACE SHANGHAI, Volume. 41, Issue 5, 90(2024)

Research and Analysis of Thermal Control Technology for Mars Surface Takeoff and Ascent

Jin YANG*... Tongjie LIU, Liang XU, Song SHENG, Haowei NI, Ai DU, Hongkang MIAO, Tao XU, Wei WANG, Zhiliang WU and Hong ZHU |Show fewer author(s)
Author Affiliations
  • Shanghai Institute of Satellite Engineering, Shanghai201109, China
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    Figures & Tables(11)
    Surface temperature curve of Mars near the SpiritMars rover[7]
    Solar radiation heat flux curve near the Spirit Mars rover[7]
    Configuration diagram of the Opportunity Mars rover[11]
    Configuration diagram of the Curiosity Mars rover[12]
    Installation method ofan instrument in the cabinet[12]
    Installation diagram of the RTG on the Perseverance Mars rover
    Configuration diagram of the Zhurong Mars rover[9]
    Configuration diagram of the insulation shell of the MAV[16]
    The heating zonesof the MAV[16]
    Physical picture of the silica nano-aerogel
    • Table 1. Comparison of the main thermal control measures for Mars rovers

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      View in Article

      Table 1. Comparison of the main thermal control measures for Mars rovers

      序号火星车主要热控手段主要优点
      1机遇号(勇气号)

      采用太阳帆板供电,火星车箱体采用厚25 mm二氧化硅气凝胶隔热,

      利用加热器低温补偿

      热控简单,质量较小,

      但适应能力较弱

      2好奇号

      采用同位素供电,火星车箱体采用机械泵驱动流体回路传热,

      利用加热器低温补偿

      热控适应能力强,但质量较大,

      所需功率较大

      3毅力号

      采用同位素供电,火星车箱体采用机械泵驱动流体回路传热,

      利用加热器低温补偿

      热控适应能力强,但质量较大,

      所需功率较大

      4祝融号

      采用太阳帆板供电,火星车箱体采用二氧化硅气凝胶隔热,

      利用加热器低温补偿

      热控简单,质量较小,

      但适应能力较弱

      5MAV

      通过平台采用蓄电池供电,MAV箱体采用二氧化硅气凝胶隔热,

      利用加热器低温补偿,器体气动热防护

      热控简单,质量较小,

      但适应能力较弱

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    Jin YANG, Tongjie LIU, Liang XU, Song SHENG, Haowei NI, Ai DU, Hongkang MIAO, Tao XU, Wei WANG, Zhiliang WU, Hong ZHU. Research and Analysis of Thermal Control Technology for Mars Surface Takeoff and Ascent[J]. AEROSPACE SHANGHAI, 2024, 41(5): 90

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    Paper Information

    Category: Deep-Space Exploration

    Received: Aug. 20, 2024

    Accepted: --

    Published Online: Jan. 15, 2025

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.05.009

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