Laser & Optoelectronics Progress, Volume. 62, Issue 9, 0922003(2025)

Non-Interface Gravity Unloading Method for Large Aperture Off-Axis Space Telescopes

Qijia He1,2,3、*, Qi Peng1,2,3,4, Zhiyun Hou1,2,3, Qihong Bao1,2,3, and Zhikun Yang1,2,3
Author Affiliations
  • 1National Key Laboratory of Optical Field Manipulation Science and Technology, Chinese Academy of Sciences,Chengdu 610209, Sichuan , China
  • 2Key Laboratory of Beam Control, Chinese Academy of Sciences, Chengdu 610209, Sichuan , China
  • 3Institute of Optics and Electronics, Chinese Academy of Sciences, Chengdu 610209, Sichuan , China
  • 4University of Chinese Academy of Sciences, Beijing 100049, China
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    Figures & Tables(15)
    Bottom view of ground test status
    Simulation result of support reaction moment
    Distribution of three unloading forces under the cross section
    Optimal distribution of unloading forces
    Iteration process of Isight optimization
    Optimized results in Pareto chart
    Topological optimization results of main support structure
    Structure of the main support frame
    Universal constant force support mechanism
    Universal constant force support mechanism
    Rotational arc cutting on contact surface
    Stress distribution before and after optimization of contact surface. (a) Before optimization; (b) after optimization
    • Table 1. Position and attitude of primary and secondary mirrors under gravity

      View table

      Table 1. Position and attitude of primary and secondary mirrors under gravity

      ItemΔX /μmΔY /μmΔZ /μm

      Δθx /

      (″)

      Δθy /

      (″)

      Δθz /

      (″)

      Primary mirror0.045.30.02.90.0-15.9
      Secondary mirror0.189.50.04.60.1-25.4
      Difference value0.144.20.01.70.19.5
    • Table 2. Method of gravity unloading

      View table

      Table 2. Method of gravity unloading

      Sling suspensionMulti-point suspensionMulti-point vertical supportMulti-point normal supportTop suspension + normal support
      Does not change the original structureRequires additional suspension pointsRequires additional horizontal surfacesDoes not change the original structureRequires additional suspension points
      Large volumeLarge volumeSmall volumeSmall volumeLarge volume
      Poor unloading effectModerate unloading effectGood unloading effectModerate unloading effectBest unloading effect
    • Table 3. Position and attitude of primary and secondary mirrors after unloading

      View table

      Table 3. Position and attitude of primary and secondary mirrors after unloading

      ItemΔX /μmΔY /μmΔZ /μm

      Δθx /

      (″)

      Δθy /

      (″)

      Δθz /

      (″)

      Primary mirror0.636.2-0.20.40.1-2.6
      Secondary mirror-4.040.8-1.20.9-1.1-4.8
      Difference value4.64.61.00.51.22.2
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    Qijia He, Qi Peng, Zhiyun Hou, Qihong Bao, Zhikun Yang. Non-Interface Gravity Unloading Method for Large Aperture Off-Axis Space Telescopes[J]. Laser & Optoelectronics Progress, 2025, 62(9): 0922003

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    Paper Information

    Category: Optical Design and Fabrication

    Received: Aug. 14, 2024

    Accepted: Sep. 23, 2024

    Published Online: May. 6, 2025

    The Author Email: Qijia He (272300602@qq.com)

    DOI:10.3788/LOP241843

    CSTR:32186.14.LOP241843

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