Infrared and Laser Engineering, Volume. 51, Issue 4, 20210496(2022)

Analysis and elimination of adhesive bonding force of flexible supported space mirror

Yongjian Wu1...2, Yong Liu1,2, and Xin Sun12 |Show fewer author(s)
Author Affiliations
  • 1Beijing Institute of Space Mechanics & Electricity, Beijing 100094, China
  • 2Beijing Key Laboratory of Advanced Optical Remote Sensing Technology, Beijing 100094, China
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    References(15)

    [1] [1] Wang Kejun, Dong Jihong, Zhou Pingwei, et al. Back suppt structure design of mirr of space remote sens [J]. Infrared Laser Engineering, 2019, 48(7): 0718004. (in Chinese)

    [2] [2] Li Yewen, Li Zongxuan, Liu Ruijing, et al. Integrated optimization design of rectangular mirr f space optical remote sens [J]. Science Technology Engineering, 2019, 19(35): 375381.

    [3] Bei Liu, Wei Wang, Yanjun Qu, et al. Design of an adjustable bipod flexure for a large-aperture mirror of a space camera. Applied Optics, 57, 4048-4055(2018).

    [4] Yueming Wang, Jianyu Wang. Image motion model and compensation methods of spaceborne opto-mechanical scanner. Infrared and Laser Engineering, 41, 952-957(2012).

    [5] [5] Yan Conglin, Wu Qinzhang, Liu Weilin. Design analysis f the suppt of large aperture rectangular mirr[J]. OptoElectronic Engineering, 2013, 40(3): 135141. (in Chinese)

    [6] [6] Chen Hongda, Chen Yonghe, Shi Tingting, et al. Lightweight mounting design f primary mirr in space camera[J]. Infrared Laser Engineering, 2014, 43(2): 535540. (in Chinese)

    [7] Qiang Liu, Xin He, Feng Zhang. Choice of adhesive applying in pointing prism for aerospace optics remote sensor. Infrared and Laser Engineering, 43, 183-187(2014).

    [8] [8] Ma Yao. Offloading capacity analysis of bipod flexure in space mirr assembly[J]. Spacecraft Recovery & Remote Sensing, 2013, 34(3): 7480. (in Chinese)

    [9] N Lobontiun, J S N Painejsn, E O’Malleye, et al. Parabolic and hyperbolic flexure hinges: flexibility, motion precision and stress characterization based on compliance closed form equations. Precision Engineering, 26, 183-192(2002).

    [10] Junfeng Hu, Yazhou Hao, Guiyang Xu. Comparative analysis of temperature effects on four kinds of flexure hinges. Journal of Mechanical Strength, 38, 144-150(2016).

    [11] [11] Zhou Xiaohua, Xing Hui, Yang Jukui. Epoxy ion f reflect mirr assembly in space remote sens [J]. Spacecraft Recovery & Remote Sensing, 2019, 40(3): 6572. (in Chinese)

    [12] [12] Li Shuang. The study of bonding stress in the epoxy bonded ultrathin optical reflect[D]. Nanjing: Southeast University, 2014. (in Chinese)

    [13] Jiawen Yang, Qiaolin Huang. Optimized design of structure parameters for large aperture mirrors. Chinese Space Science and Technology, 31, 77-83(2011).

    [14] Deyi Dong, Zhilai Li, Ruigang Li, et al. Simulation and experiment of influence of adhesive curing on refective mirror surface. Optics and Precision Engineering, 22, 2698-2707(2014).

    [15] Yuting Lu, Weizhi Wang. Alignment of large aperture gluing primary mirror with finite element method. Spacecraft Recovery & Remote Sensing, 38, 38-44(2017).

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    [1] Bin Li, Sisi Gao, Haichao Wang, Jiayi Chen, Xi Chen, Yuting Lu. Adjustment and testing method of large aperture mirror Bipod support structure[J]. Infrared and Laser Engineering, 2024, 53(4): 20230657

    [2] Yingchao Li, Qing Zhang, Zhuang Liu, Haodong Shi, Qiang Fu. Design of automatic out-of-focus correction system for near-space lidar receivers[J]. Infrared and Laser Engineering, 2024, 53(4): 20230645

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    Yongjian Wu, Yong Liu, Xin Sun. Analysis and elimination of adhesive bonding force of flexible supported space mirror[J]. Infrared and Laser Engineering, 2022, 51(4): 20210496

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    Paper Information

    Category: Optical design

    Received: Jul. 19, 2021

    Accepted: --

    Published Online: May. 18, 2022

    The Author Email:

    DOI:10.3788/IRLA20210496

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