• Infrared and Laser Engineering
  • Vol. 53, Issue 8, 20240274 (2024)
Xu LIU, Heng WANG, Xiaofeng LIU, and Zhen JIA
Author Affiliations
  • Research and Design Department, Changchun Nationspace Optics Technology Co., Ltd., Changchun 130000, China
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    DOI: 10.3788/IRLA20240274 Cite this Article
    Xu LIU, Heng WANG, Xiaofeng LIU, Zhen JIA. Design and analysis of carbon fiber main load-bearing cylinder structure for space cameras[J]. Infrared and Laser Engineering, 2024, 53(8): 20240274 Copy Citation Text show less
    References

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    [2] Xiaoyong WANG, Chongling GUO, Yongli HU. Design and ver-ification for front mirror-body structure of on-axis three mirror anastigmatic space camera. Acta Photonica Sinica, 40, 34-40(2011).

    [3] Renzhang ZHU. Global high-resolution optical satellite overview(1): USA and Canada. Spacecraft Engineering, 24, 85-106(2015).

    [4] Tailei WANG. Optimization design of integrated ultra light main support structure for micro nano remote sensing cameras. Acta Optica Sinica, 39, 0728009(2019).

    [5] XIN H W, LI Z L. Structural design f light weighting off axis TMA space scope [C]2011 Second International Conference on Digital Manufacturing & Automation, IEEE, 2011: 11251128.

    [6] Lei WEI. Optimization design and experiment of the front frame of a large off-axis three mirror space camera. Acta Photonica Sinica, 46, 0522001(2017).

    [7] Yingjun GUAN. Topological optimization design of the main support structure for space cameras. Optics and Precision Engineering, 15, 1157-1163(2007).

    [8] Xunpeng SONG. Carbon fiber thin-walled cylindrical primary and secondary mirror support structure for space cameras. Optics and Precision Engineering, 30, 1429-1439(2022).

    [9] Yongxian WANG, Bing WANG, Jianyue REN. Improvement of carbon fiber support structure and topology optimization design of space camera. Infrared and Laser Engineering, 38, 702-724(2009).

    [10] Ling LI, Ye ZHAO. Gravity unloading method for ground installation and adjustment of large aperture space cameras. Spacecraft Recovery & Remote Sensing, 37, 69-76(2016).

    [11] WEI Lei. Optimization design of main suppt structure of long focal length wide field of view space camera [D]. Changchun: Changchun Institute of Optics, Fine Mechanics Physics, Chinese Academy of Sciences, 2017. (in Chinese)

    [12] Weiwei XU, Wei WEN, Yayuan LI. Effect of different process conditions on interlayer properties of M40J carbon fiber/bismaleic resin matrix composite materials. Plastic Industry, 50, 76-81(2022).

    [13] Jianshe WANG. Dynamic environmental testing of space optical components. Optics and Precision Engineering, 9, 174-176(2001).

    [14] CAO Minghui. Lightweight design of carbon fiber integrated main frame f micro space camera [D]. Changchun: Changchun Institute of Optics, Fine Mechanics Physics, Chinese Academy of Sciences, 2022. (in Chinese)

    [15] KE Shanxin. Optimization design of main suppt structure of ultra light space camera [D]. Changchun: Changchun Institute of Optics, Fine Mechanics Physics, Chinese Academy of Sciences, 2018. (in Chinese)

    [16] SUN Baoyu. Research on the dynamic acteristics of lightweight large field optical remote sensing sens structure [D]. Changchun: Changchun Institute of Optics, Fine Mechanics Physics, Chinese Academy of Sciences, 2004. (in Chinese)

    [17] YANG Lin. Large swath high resolution satellite integrated structure multiobjective optimization design [D]. Beijing: Chinese Academy of Sciences, 2019. (in Chinese)

    Xu LIU, Heng WANG, Xiaofeng LIU, Zhen JIA. Design and analysis of carbon fiber main load-bearing cylinder structure for space cameras[J]. Infrared and Laser Engineering, 2024, 53(8): 20240274
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