• Acta Photonica Sinica
  • Vol. 50, Issue 4, 207 (2021)
Weiyan LI1、2, Qunbo LÜ1、2、3, Yangyang LIU1、2、3, Zheng TAN1、2, Jianwei WANG1、2, Na ZHAO1、2、3, Linlin PEI1、2, Jianying SUN1、2, and Xinwen CHEN1、2
Author Affiliations
  • 1Aerospace Information Research Institute, Chinese Academy of Sciences, Beijing00094, China
  • 2Key Laboratory of Computational Optical Imagine Technology, CAS, Beijing100094, China
  • 3University of the Chinese of Academy of Science, Beijing100094, China
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    DOI: 10.3788/gzxb20215004.0412001 Cite this Article
    Weiyan LI, Qunbo LÜ, Yangyang LIU, Zheng TAN, Jianwei WANG, Na ZHAO, Linlin PEI, Jianying SUN, Xinwen CHEN. Thermal Characteristics Analysis and Verification of Primary Supporting Structure for Spaceborne Camera Based on Low Volume SiC/Al Primary Mirror Frame[J]. Acta Photonica Sinica, 2021, 50(4): 207 Copy Citation Text show less
    Supporting structures used for spaceborne camera
    Fig. 1. Supporting structures used for spaceborne camera
    Optical structure used for verification
    Fig. 2. Optical structure used for verification
    Three-dimensional structure of primary mirror frame
    Fig. 3. Three-dimensional structure of primary mirror frame
    Topology optimization of primary mirror frame
    Fig. 4. Topology optimization of primary mirror frame
    Optimized primary mirror frame
    Fig. 5. Optimized primary mirror frame
    Primary mirror deformation (TC4 primary frame)
    Fig. 6. Primary mirror deformation (TC4 primary frame)
    Primary mirror deformation (SiC/Al primary frame)
    Fig. 7. Primary mirror deformation (SiC/Al primary frame)
    TC4 primary mirror frame temperature
    Fig. 8. TC4 primary mirror frame temperature
    SiC/Al primary mirror frame temperature
    Fig. 9. SiC/Al primary mirror frame temperature
    Camera MTF (TC4 primary mirror frame)
    Fig. 10. Camera MTF (TC4 primary mirror frame)
    Camera MTF (SiC/Al primary mirror frame)
    Fig. 11. Camera MTF (SiC/Al primary mirror frame)
    Position of main frame temperature measuring point
    Fig. 12. Position of main frame temperature measuring point
    Spaceborne camera thermo-optic experiment
    Fig. 13. Spaceborne camera thermo-optic experiment
    Target image of camera assembled
    Fig. 14. Target image of camera assembled
    Target image of thermo-optic experiment
    Fig. 15. Target image of thermo-optic experiment
    TypeIndex
    Orbit height/km700
    Width/km≥20
    Original spatial⁃resolution/m2.8
    Processed spatial⁃resolution/m1.4
    Spectral range/nm450~900
    Primary size/mm300
    Weight/kg≤23
    Space size/mmφ400×900
    Table 1. Spaceborne camera parameters used for verification
    Material

    Density ρ

    /(g·cm-3)

    Elastic modulus E

    /Gpa

    Thermal conductivity λ

    /(W·m-1·K)

    Coefficient of Thermal expansionα/(×10-6-1)
    Al2.787012022.7
    TC44.441146.89.2
    15%SiC/Al2.849714017
    4J328.114113.90.65
    Table 2. Material properties for spaceborne camera
    Material

    Specific stiffness

    E/ρ

    Thermal stability

    λ/α

    Performance factors

    (E/ρ)(λ/α)

    Al25.25.3133.6
    TC425.70.718
    15%SiC/Al34.28.2280.4
    4J3217.421.4372.4
    Table 3. Material Performance factors
    Measuring point 1Measuring point 2Measuring point 3Average temperature/℃
    22.021.822.222.0
    21.921.622.121.9
    21.821.622.021.8
    21.621.421.921.6
    21.621.421.821.6
    21.120.921.221.1
    21.120.921.321.1
    21.121.021.321.1
    21.321.121.421.3
    21.321.121.521.3
    21.521.321.621.5
    Table 4. Temperature date of primary mirror frame thermo-optic experiment
    Weiyan LI, Qunbo LÜ, Yangyang LIU, Zheng TAN, Jianwei WANG, Na ZHAO, Linlin PEI, Jianying SUN, Xinwen CHEN. Thermal Characteristics Analysis and Verification of Primary Supporting Structure for Spaceborne Camera Based on Low Volume SiC/Al Primary Mirror Frame[J]. Acta Photonica Sinica, 2021, 50(4): 207
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