Acta Photonica Sinica, Volume. 53, Issue 12, 1222003(2024)

Precision Thermal Control of High Resolution Micro-satellite of Platform and Payload Integration

Tian BAI1...2, Feng JIANG1, Lin KONG1,*, Lei ZHANG1 and Jianchao WANG1 |Show fewer author(s)
Author Affiliations
  • 1Chang Guang Satellite Technology Co.,Ltd.Changchun 130000,China
  • 2School of Mechatronics Engineering,Harbin Institute of Technology,Harbin 150000,China
  • show less
    Figures & Tables(19)
    Overall layout of the satellite
    Heat flow analysis results
    Temperature control of reflective mirror
    Temperature fluctuation of mirror heater
    Temperature control of truss
    Temperature control of focal plane
    Installation of the phase change material
    Heat dissipation of electronic components
    Numerical analysis model
    Thermal balance test model
    The situation of thermal balance test
    The distribution of heat flux meters
    Temperature of the mirror in orbit
    Temperature of truss in orbit
    Temperature of CCD
    • Table 1. Technical indicators of the thermal control

      View table
      View in Article

      Table 1. Technical indicators of the thermal control

      ComponentsThermal control target
      Camera lens19.5~20.5 ℃,temperature fluctuation shall not exceed±0.1 ℃
      CCDs10~20 ℃,temperature rise during imaging<1 ℃/min
      Battery10~30 ℃
    • Table 2. Temperature calculation results

      View table
      View in Article

      Table 2. Temperature calculation results

      ComponentsCold case/℃Hot case/℃
      Mirrors19.8~20.119.8~20.1
      Truss19.8~20.219.8~20.2
      CCDs14.5~15.517~20
      Battery18.5~2018.5~20
      Propulsion system(tank)5.5~6.517~21
      Avionics8.4~1221~29
    • Table 3. Heat flux data for each region and the temperature of heat flux meters

      View table
      View in Article

      Table 3. Heat flux data for each region and the temperature of heat flux meters

      PositionHeat flux meter codeHeat flux in summer solstice/(W·m-2

      Controlled temperature of heat flux

      meter/℃

      Heat flux in winter solstice/(W·m-2Controlled temperature of heat flux meter/℃
      +X heat flux of platformQ1133-3029422
      +X heat flux of cameraQ2133-3029422
      -X heat flux of platformQ387-5494-38
      -X heat flux of cameraQ488-5494-38
      +Y heat flux of platformQ539-7848-66
      +Y heat flux of cameraQ639-6048-47
      -Y heat flux of platformQ745-8065-65
      -Y heat flux of cameraQ845-5662-38
      -Z heat flux of platformQ947-9680-65
      +Z heat flux of cameraQ10147-47165-33
    • Table 4. Test and in-orbit temperature data

      View table
      View in Article

      Table 4. Test and in-orbit temperature data

      ComponentsCold case during test/℃Hot case during test/℃Temperature in flight/℃
      Mirrors19.8~20.219.8~20.219.9~20.2
      Truss19.8~20.319.8~20.319.9~20.3
      CCDs14.5~15.515.5~20.015.0~19.8
      Battery18.5~20.018.5~20.520.0~23.0
      Propulsion system(tank)5.5~6.515.0~19.012.0~16.0
      Avionics6.0~9.020.0~28.022.0~32.0
    Tools

    Get Citation

    Copy Citation Text

    Tian BAI, Feng JIANG, Lin KONG, Lei ZHANG, Jianchao WANG. Precision Thermal Control of High Resolution Micro-satellite of Platform and Payload Integration[J]. Acta Photonica Sinica, 2024, 53(12): 1222003

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category: Optical Design and Fabrication

    Received: May. 27, 2024

    Accepted: Sep. 13, 2024

    Published Online: Jan. 15, 2025

    The Author Email: KONG Lin (konglin@charmingglobe.com)

    DOI:10.3788/gzxb20245312.1222003

    Topics