Infrared and Laser Engineering, Volume. 50, Issue 4, 20200294(2021)

Thermal design of space solar telescope

Shuang Yang1...2, Changshuai Du3, Xianwei Yang1, Chunlong Liu1, and Yan Xiong12 |Show fewer author(s)
Author Affiliations
  • 1Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China
  • 2University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, Beijing 100049, China
  • show less
    Figures & Tables(18)
    Schematic diagram of the overall structure of the space solar telescope
    Thermal control system composition diagram
    Schematic diagram of implementation state of frame
    Guide telescope cooling path diagram
    Finite element thermal analysis model
    Thermal equilibrium test device and platform
    Thermal analysis cloud of frame (a) and guide telescope (b) under high temperature conditions
    Comparison curve between simulation and test under high temperature conditions
    Thermal analysis cloud of frame (a) and guide telescope (b) under low temperature conditions
    Comparison curve between simulation and test under low temperature conditions
    • Table 1. [in Chinese]

      View table
      View in Article

      Table 1. [in Chinese]

      ComponentOperating temperature/℃Thermal control index/℃
      Frame19-2522±1
      Guiding telescope19-2522±1
    • Table 2. [in Chinese]

      View table
      View in Article

      Table 2. [in Chinese]

      Operating modeWorking stateParameter setting
      High temperatureGuide mirror operation (Balanced condition)a) The telescope is in a high temperature external heat flow, the solar constant is 1412 W/m2; b) Thermal control coating takes end-of-life value; c) The 87° light angle guide is oriented to the sun.
      Low temperatureGuide mirror operation (Balanced condition)a) The telescope is in a high temperature external heat flow, the solar constant is 1322 W/m2; b) Thermal control coating takes initial value of life; c) The 57° light angle guide is oriented to the sun.
    • Table 3. [in Chinese]

      View table
      View in Article

      Table 3. [in Chinese]

      ComponentMaterialDensity/kg·m−3Specific heat capacity/ J·(kg·℃)−1Thermal conductivity/W·(m· ℃)−1
      FrameAluminium alloy 7A092800921154
      Guiding telescopeAluminium alloy 2A122800920121
    • Table 4. [in Chinese]

      View table
      View in Article

      Table 4. [in Chinese]

      Num.Component nameDesign statusTest statusConsistency analysis
      1FrameAluminium alloy 7A09Aluminium alloy 7A09Accordance
      2Guiding telescopeAluminium alloy 2A12Aluminium alloy 2A12Accordance
      3Temperature measurement sensorThermistorThermocoupleMeet the test requirements
      4Thermal conductive fillerThermal greaseThermal greaseAccordance
      5Heat insulation material20-unit multilayer insulation assembly (Mask is F46 film) 20-unit multilayer insulation assembly (Mask is F46 film) Accordance
      6Heater125 type polyimide film heater125 type polyimide film heaterAccordance
    • Table 5. [in Chinese]

      View table
      View in Article

      Table 5. [in Chinese]

      PositionWorking power/WWorking voltage/VTotal circuit resistance/Ω
      Upper cover plate103090
      Lower cover plate7.7730115.8
      Upper of mounting substrate − Y730128.6
      Upper of mounting substrate +Y730128.6
      Lower of mounting substrate − Y7.2530124.1
      Lower of mounting substrate +Y6.9530129.5
    • Table 6. [in Chinese]

      View table
      View in Article

      Table 6. [in Chinese]

      No.PositionSensor code
      1Frame +XTR-TBZX
      2Frame − XTR-TBFX
      3Upper cover plateTR-SGB
      4Lower cover plateTR-XGB
      5Upper of mounting substrate − YTR-SFY
      6Upper of mounting substrate +YTR-SZY
      7Lower of mounting substrate − YTR-XFY
      8Lower of mounting substrate +YTR-XZY
      9Guiding telescopeTR-DXJ
    • Table 7. [in Chinese]

      View table
      View in Article

      Table 7. [in Chinese]

      No.Heating zoneFinite element simulation analysis of average power consumption/WThermal equilibrium test average power consumption/W
      1Upper cover plate1.01.1
      2Lower cover plate00
      3Upper of mounting substrate -Y6.36.7
      4Upper of mounting substrate +Y6.16.5
      5Lower of mounting substrate -Y3.63.8
      6Lower of mounting substrate +Y3.84.0
      7Guiding telescope3.23.1
      8Summation2425.2
    • Table 8. [in Chinese]

      View table
      View in Article

      Table 8. [in Chinese]

      No.Heating zoneFinite element simulation analysis of average power consumption/WThermal equilibrium test average power consumption/W
      1Upper cover plate1.01.1
      2Lower cover plate00
      3Upper of mounting substrate -Y7.36.7
      4Upper of mounting substrate +Y7.16.6
      5Lower of mounting substrate -Y3.63.9
      6Lower of mounting substrate +Y3.83.7
      7Guiding telescope3.23.2
      8Summation2625.2
    Tools

    Get Citation

    Copy Citation Text

    Shuang Yang, Changshuai Du, Xianwei Yang, Chunlong Liu, Yan Xiong. Thermal design of space solar telescope[J]. Infrared and Laser Engineering, 2021, 50(4): 20200294

    Download Citation

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

    Category: Optical design

    Received: Aug. 4, 2020

    Accepted: --

    Published Online: Jul. 30, 2021

    The Author Email:

    DOI:10.3788/IRLA20200294

    Topics