Chinese Optics, Volume. 15, Issue 5, 1079(2022)

Flexural mounting technology of a 1.8 m space-borne rectangular mirror

Zong-xuan LI1,3、*, Chang-hao ZHANG1,2,3, De-fu ZHANG1,3, Bin MA1,2,3, and Yun-feng LI1,2,3
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
  • 3Key Laboratory of Space-Based Dynamic Fast Optical Imaging Technology, Chinese Academy of Sciences, Changchun 130033, China
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    References(14)

    [1] JI H R, ZHU ZH B, TAN H, et al. Design of a high-throughput telescope based on scanning an off-axis three-mirror anastigmat system[J]. Applied Optics, 60, 2817-2823(2021).

    [2] LI Y W, LI Z X, LIU R J, . Integrated optimization design of rectangular mirror for space optical remote sensor[J]. Science Technology and Engineering, 19, 375-381(2019).

    [3] LI Z X, CHEN X, ZHANG L, . Design of Cartwheel flexural support for a large aperture space mirror[J]. Acta Optica Sinica, 34, 0622003(2014).

    [4] QU H D, WEI J L, DONG D Y, . Lightweight structural design of rectangular space mirror assembly[J]. Infrared and Laser Engineering, 50, 20200404(2021).

    [5] KIHM H, YANG H S. Design optimization of a 1-m lightweight mirror for a space telescope[J]. Optical Engineering, 52, 091806(2013).

    [6] ZHU J Q, SHA W, CHEN CH ZH, . Position layout of rear three point mounting for space rectangular mirror[J]. Optics and Precision Engineering, 23, 2562-2569(2015).

    [7] HUO T L, YU J J, ZHAO H ZH. Design of a kinematic flexure mount for precision instruments based on stiffness characteristics of flexural pivot[J]. Mechanism and Machine Theory, 150, 103868(2020).

    [8] WANG P P, XIN H W, ZHU J Q, . Parametric optimization design of rectangular reflective mirror and flexible component[J]. Infrared and Laser Engineering, 50, 20200493(2021).

    [9] LIU F H, CHENG ZH F, SHI L, . Design and analysis of supporting structure for rectangular mirror[J]. Infrared and Laser Engineering, 44, 1512-1517(2015).

    [10] YANG Q SH, ZHANG J Y, YU J H, . Research on error analysis of support deformation for large aperture space mirrors[J]. Spacecraft Recovery & Remote Sensing, 41, 60-70(2020).

    [11] LIU X H, LI SH CH, LI M X, . Supporting structure design for primary and tertiary mirror of off-axis TMA system[J]. Infrared and Laser Engineering, 50, 20210025(2021).

    [12] [12] KRUIS J R C G. Design, analysis, testing applications of twobody threebody kinematic mounts[D]. Lausanne: cole Polytechnique Fédérale de Lausanne, 2016.

    [13] [13] HOWELL L L, MAGLEBY S P, OLSEN B M. Hbook of Compliant Mechanisms[M]. CHEN G M, YU J J, MA H B, et al. , trans. Beijing: Higher Education Press, 2015. (in Chinese)

    [14] LI Z X, CHEN X, WANG SH J, et al. Optimal design of a Φ760 mm lightweight SiC mirror and the flexural mount for a space telescope[J]. Review of Scientific Instruments, 88, 125107(2017).

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    Zong-xuan LI, Chang-hao ZHANG, De-fu ZHANG, Bin MA, Yun-feng LI. Flexural mounting technology of a 1.8 m space-borne rectangular mirror[J]. Chinese Optics, 2022, 15(5): 1079

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    Paper Information

    Category: Original Article

    Received: Jun. 13, 2022

    Accepted: --

    Published Online: Sep. 29, 2022

    The Author Email:

    DOI:10.37188/CO.2022-0131

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