• Infrared and Laser Engineering
  • Vol. 50, Issue 6, 20200404 (2021)
Huidong Qu1, Jiali Wei1, Deyi Dong2, Haifei Hu2, and Yingjun Guan1
Author Affiliations
  • 1School of Mechanical and Electrical Engineering, Changchun University Of Technology, Changchun 130012, China
  • 2Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China
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    DOI: 10.3788/IRLA20200404 Cite this Article
    Huidong Qu, Jiali Wei, Deyi Dong, Haifei Hu, Yingjun Guan. Lightweight structural design of rectangular space mirror assembly[J]. Infrared and Laser Engineering, 2021, 50(6): 20200404 Copy Citation Text show less
    References

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    [2] Zhilai Li, Hong Xu, Yingjun Guan. Structural design of 1.5 m mirror subassenbly for space camera. Optics and Precision Engineering, 23, 1635-1641(2015).

    [3] Junqing Zhu, Wei Sha, Changzheng Chen, et al. Position layout of rear three point mounting for space rectangular mirror. Optics and Precision Engineering, 23, 2562-2569(2015).

    [4] Li Yewen. Research on lightweighting flexural mounting technology of spacebne large size rectangular mirr[D]. Changchun: University of Chinese Academy of Sciences (Changchun Institute of Optics Precision Machinery Physics, Chinese Academy of Sciences), 2020. (in Chinese)

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    [6] Yan Zhai, Huilin Jiang, Gui Mei, et al. Material selection and design of beryllium-aluminum alloy mirror assembly for large-diameter space infrared camera. Infrared and Laser Engineering, 49, 20190390(2020).

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    [8] Li Mengqing. Designs of lightweight athermal f rectangular space mirr[D]. Changchun: University of Chinese Academy of Sciences (Changchun Institute of Optics Precision Machinery Physics), 2015. (in Chinese)

    [9] Bing San, Jinglin Li, Bin Sun. Light-weight technology and its application of large-aperture mirror in space camera. Infrared and Laser Engineering, 44, 3043-3048(2015).

    [10] Yoder P R. OptoMechanical Systems Design. 3rd ed [M]OptoMechanical Systems Design. Third Edition, Boca Raton: CRC Press, Inc., 2005.

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    [12] Vukobratovich D, Iraninejad B, Rid R M. Optimum shapes f lightweighted mirrs[C]Proceedings of SPIEThe International Society f Optical Engineering, 1982, 332(12): 419423.

    [13] Kejun Wang, Ming Xuan, Jihong Dong, et al. Design method of reflector component structure of space remote sensor. Infrared and Laser Engineering, 45, 1113001(2016).

    [14] Hong Xu, Yingjun Guan. Structural design of 1 m diameter space mirror component of space camera. Optics and Precision Engineering, 21, 1488-1495(2013).

    [15] Yingfei Wu, Zhaoying Zhou. Design of flexible hinges. Engineering Mechanics, 19, 136-140(2002).

    [16] Xingyong Zuo, Xiaoming Liu. Calculation and analysis of rotational stiffness of three types of flexure hinges. Chinese Journal of Scientific Instrument, 24, 1725-1728(2006).

    [17] Zengyao Han, Yuanjie Zou, Weihong Zhu, et al. Evolution of the spacecraft mechanical environment predication & test technology. Scientia Sinica Physica, Mechanica & Astronomica, 49, 6-22(2019).

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    Huidong Qu, Jiali Wei, Deyi Dong, Haifei Hu, Yingjun Guan. Lightweight structural design of rectangular space mirror assembly[J]. Infrared and Laser Engineering, 2021, 50(6): 20200404
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