• Infrared and Laser Engineering
  • Vol. 53, Issue 10, 20240202 (2024)
Qiang ZHANG1, Baoyu YANG1,2,*, Zhipeng GUO1, Yuhan LI1,2..., Junfei LI1 and Yinong WU1,2|Show fewer author(s)
Author Affiliations
  • 1Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083, China
  • 2University of Chinese Academy of Sciences, Beijing 101408, China
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    DOI: 10.3788/IRLA20240202 Cite this Article
    Qiang ZHANG, Baoyu YANG, Zhipeng GUO, Yuhan LI, Junfei LI, Yinong WU. Research on optimization of temperature uniformity of spaceborne blackbody[J]. Infrared and Laser Engineering, 2024, 53(10): 20240202 Copy Citation Text show less
    (a) Schematics of structure of the blackbody; (b) Schematics of reverse side of the blackbody
    Fig. 1. (a) Schematics of structure of the blackbody; (b) Schematics of reverse side of the blackbody
    Schematics of the blackbody and surrounding structures
    Fig. 2. Schematics of the blackbody and surrounding structures
    Schematics of the thermistors embedded in the back of the blackbody
    Fig. 3. Schematics of the thermistors embedded in the back of the blackbody
    Comparison of results of experiments and simulations
    Fig. 4. Comparison of results of experiments and simulations
    Comparison of performance of 4-layer UTSs
    Fig. 5. Comparison of performance of 4-layer UTSs
    Comparison of performance of 5-layer UTSs
    Fig. 6. Comparison of performance of 5-layer UTSs
    Comparison of performance of 6-layer UTSs. (a) Using 0 or 1 layer PI; (b) Using 2 layers PI
    Fig. 7. Comparison of performance of 6-layer UTSs. (a) Using 0 or 1 layer PI; (b) Using 2 layers PI
    MaterialDensity/kg·m−3In-plane thermal conductivity/W·(m·K)−1Normal thermal conductivity/W·(m·K)−1Specific heat capacity/J·(kg·K)−1
    Al alloy (2A12)2780121121920
    Copper8900385385394
    Polyimide (PI)14110.40.41004
    Thermal pyrolytic graphite (TPG)229810918.0811
    Table 1. Thermophysical properties used in the finite element analysis
    Uniform temperaturestructureHeaterBlackbodyHeat pipeat the blackbody sideHeat pipe at the radiator sideRadiator
    0(2+1)324.418323.041322.945319.769318.203
    3(2+1)326.089323.072322.878319.639318.075
    Table 2. Analysis of cause of temperature changes of blackbody (Unit: K)
    Qiang ZHANG, Baoyu YANG, Zhipeng GUO, Yuhan LI, Junfei LI, Yinong WU. Research on optimization of temperature uniformity of spaceborne blackbody[J]. Infrared and Laser Engineering, 2024, 53(10): 20240202
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