• Infrared and Laser Engineering
  • Vol. 50, Issue 7, 20200464 (2021)
Xiang Li1、2, Dongwei Bai1、2、*, Lixin Meng1、2, Liang Gao2、3, and Yan An2、3
Author Affiliations
  • 1School of Mechanical Engineering, Changchun University of Science and Technology, Changchun 130022, China
  • 2National and Local Joint Engineering Research Center of Space and Optoelectronics Technology, Changchun University of Science and Technology, Changchun 130022, China
  • 3School of Opto Electronic Engineering, Changchun University of Science and Technology, Changchun 130022, China
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    DOI: 10.3788/IRLA20200464 Cite this Article
    Xiang Li, Dongwei Bai, Lixin Meng, Liang Gao, Yan An. Optical telescope of space debris detection and ranging compound system[J]. Infrared and Laser Engineering, 2021, 50(7): 20200464 Copy Citation Text show less
    Space debris ranging and imaging composite system
    Fig. 1. Space debris ranging and imaging composite system
    Principle diagram of the optical path of the space debris detection and ranging composite system
    Fig. 2. Principle diagram of the optical path of the space debris detection and ranging composite system
    Optical structure of telescope structure system
    Fig. 3. Optical structure of telescope structure system
    System image quality evaluation
    Fig. 4. System image quality evaluation
    Structure diagram of the main mirror assembly
    Fig. 5. Structure diagram of the main mirror assembly
    Flexible support
    Fig. 6. Flexible support
    RMS value analysis result of the surface error of the main mirror assembly
    Fig. 7. RMS value analysis result of the surface error of the main mirror assembly
    First three modes of the primary mirror assembly
    Fig. 8. First three modes of the primary mirror assembly
    Lightweight hole model of main mirror
    Fig. 9. Lightweight hole model of main mirror
    Model comparison under different lightweight shapes
    Fig. 10. Model comparison under different lightweight shapes
    Surface inspection result of main mirror assembly
    Fig. 11. Surface inspection result of main mirror assembly
    Secondary mirror assembly structure
    Fig. 12. Secondary mirror assembly structure
    Structure diagram of optical telescope
    Fig. 13. Structure diagram of optical telescope
    Simulation results of the whole machine
    Fig. 14. Simulation results of the whole machine
    Simulation results of the tail installation of the whole machine
    Fig. 15. Simulation results of the tail installation of the whole machine
    Surface fitting results
    Fig. 16. Surface fitting results
    Testing site
    Fig. 17. Testing site
    Test of the optical telescope surface shape error
    Fig. 18. Test of the optical telescope surface shape error
    ItemTechnical index requirements
    Effective aperture of optical system250 mm
    Surface accuracy RMS of main mirror assemblyλ/40
    System wave aberration RMSλ/10
    Primary and secondary mirror spacing error≤0.02 mm
    Primary and secondary mirror tilt≤3″
    Secondary mirror and bracket blocking ratio≤7%
    Optical antenna fundamental frequency≥120 Hz
    Optical antenna quality≤10 kg
    Table 1. Technical specificatons optical telescope
    Material$\rho /{g}\cdot {\rm cm}^{-3}$$ E/\rho $Thermal stability$ \mu $$ \mathrm{\alpha }/ $
    Zerodur2.533.5832.80.230.05 $ \times {10}^{-6} $
    Be1.8515.619.120.2611.3 $ \times {10}^{-6} $
    RB-SIC3.510.660.70.292.6 $ \times {10}^{-6} $
    Al2.682.557.10.3323.6 $ \times {10}^{-6} $
    ULE2.213.0887.30.170.015 $ \times {10}^{-6} $
    TC42.534.4429.490.238.9 $ \times {10}^{-6} $
    4J328.11746.330.260.3 $ \times {10}^{-6} $
    4J368.05188.250.291.26 $ \times {10}^{-6} $
    2A122.9277.10.3323.6 $ \times {10}^{-6} $
    60SiC/Al3.027125.880.178.5 $ \times {10}^{-6} $
    Table 2. Material properties of optical telescope
    Structure typeTrianglecircleHexagon
    Minimum thickness/mm8.99.29.5
    Table 3. Minimum panel thickness required for different lightweight structures
    Structure typeFirst-order modeSecond-order modeThird-order modeQuality/kgLightweight rateVolume/mm3Surface area/mm2
    Triangle2290.32290.529762.49240.62%9.95e+052.57e+05
    Circle2005.42010.226982.42242.28%9.58e+052.15e+05
    Hexagon1870.41890.625012.40142.72%9.54e+052.02e+05
    Table 4. Lightweight analysis results of main mirror
    Xiang Li, Dongwei Bai, Lixin Meng, Liang Gao, Yan An. Optical telescope of space debris detection and ranging compound system[J]. Infrared and Laser Engineering, 2021, 50(7): 20200464
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