Optics and Precision Engineering, Volume. 29, Issue 12, 2877(2021)

Design and analysis of the repeatable development and collapse mechanism film protective cover of space camera

Hong XIAO1... Hong-yang WANG1, Hong-wei GUO1,*, Sai ZHANG2, Rong-qiang LIU1, Bin FAN3 and Jiang BIAN3 |Show fewer author(s)
Author Affiliations
  • 1State Key Laboratory of Robotics and System, Harbin Institute of Technology,Harbin5000, China
  • 2Tiandi Technology Co., Ltd., Beijing10000, China
  • 3Institute of Optics and Electronics, Chinese Academy of Sciences, Chengdu610207, China
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    References(19)

    [1] [1] 1张立超, 高劲松. 长春光机所深紫外光学薄膜技术研究进展[J]. 光学 精密工程, 2012, 20(11): 2395-2401. doi: 10.3788/ope.20122011.2395ZHANGL CH, GAOJ S. Developments of DUV coating technologies in CIOMP[J]. Opt. Precision Eng., 2012, 20(11): 2395-2401. (in Chinese). doi: 10.3788/ope.20122011.2395

    [2] [2] 2高明星, 刘荣强, 李冰岩, 等. 空间可展开三棱柱伸展臂设计与优化[J]. 机械工程学报, 2020, 56(15): 129-137. doi: 10.3901/jme.2020.15.129GAOM X, LIUR Q, LIB Y, et al. Design and optimization of space deployable tri-prism mast[J]. Journal of Mechanical Engineering, 2020, 56(15): 129-137. (in Chinese). doi: 10.3901/jme.2020.15.129

    [3] [3] 3叶钊, 李熹微, 王超, 等. 微纳卫星光学载荷技术发展综述[J]. 航天器工程, 2016, 25(6): 122-130. doi: 10.3969/j.issn.1673-8748.2016.06.019YEZH, LIX W, WANGCH, et al. Survey of technological development of optical payload for micro-nano satellite[J]. Spacecraft Engineering, 2016, 25(6): 122-130. (in Chinese). doi: 10.3969/j.issn.1673-8748.2016.06.019

    [4] [4] 4李玉高, 傅丹膺, 王永辉. 空间光学精密展开机构多功能铰锁的发展[J]. 宇航学报, 2008, 29(4): 1090-1093, 1111. doi: 10.3873/j.issn.1000-1328.2008.04.002LIY G, FUD Y, WANGY H. Develop on multifunctional hinge and latch of space optical-precision deployable instruments[J]. Journal of Astronautics, 2008, 29(4): 1090-1093, 1111. (in Chinese). doi: 10.3873/j.issn.1000-1328.2008.04.002

    [5] [5] 5徐明林, 徐伟, 帅智艳, 等. 一种用于空间相机的高精度线性调焦机构[P]. 吉林省:CN108073015B, 2020-03-13.XUM L, XUW, SHUAIZH Y, et al. A High-precision Linear Focusing Mechanism for Space Cameras[P]. Jilin Province: CN108073015B, 2020-03-13. (in Chinese)

    [6] [6] 6陈立恒, 吴清文, 刘伟奇, 等. 空间摄像机热控系统设计[J]. 光学 精密工程, 2012, 20(3): 556-562. doi: 10.3788/OPE.20122003.0556CHENL H, WUQ W, LIUW Q, et al. Thermal design for space cameras[J]. Opt. Precision Eng., 2012, 20(3): 556-562. (in Chinese). doi: 10.3788/OPE.20122003.0556

    [7] [7] 7牛晓明, 卢锷, 赵鹏. 空间光学系统的热分析[J]. 光学 精密工程, 1996, 4(6): 56-62. doi: 10.3321/j.issn:1004-924X.1996.06.010NIUX M, LUE, ZHAOP. Thermal analysis of space optical system[J]. Opt. Precision Eng., 1996, 4(6): 56-62. (in Chinese). doi: 10.3321/j.issn:1004-924X.1996.06.010

    [8] [8] 8江经善. 多层隔热材料及其在航天器上的应用[J]. 宇航材料工艺, 2000, 30(4): 17-25. doi: 10.3969/j.issn.1007-2330.2000.04.004JIANGJ SH. Multilayer insulation materials and their application to spacecrafts[J]. Aerospace Materials & Technology, 2000, 30(4): 17-25. (in Chinese). doi: 10.3969/j.issn.1007-2330.2000.04.004

    [9] [9] 9林秋红, 张骞, 贾文文, 等. 大型空间薄膜遮阳罩折展构型设计与分析[J]. 机械工程学报, 2020, 56(5): 13-20. doi: 10.3901/JME.2020.05.013LINQ H, ZHANGQ, JIAW W, et al. Deployable configuration design and analysis of large space membrane sunshield structures[J]. Journal of Mechanical Engineering, 2020, 56(5): 13-20. (in Chinese). doi: 10.3901/JME.2020.05.013

    [10] J ARENBERG, J FLYNN, A COHEN et al. Status of the JWST sunshield and spacecraft, 9904, 20-33(2016).

    [11] [11] 11王长杰, 杨居奎, 孙立, 等. “高分七号”卫星双线阵相机的设计及实现[J]. 航天返回与遥感, 2020, 41(2): 29-38.WANGCH J, YANGJ K, SUNL, et al. Design and implementation of the dual line array camera for GF-7 satellite[J]. Spacecraft Recovery & Remote Sensing, 2020, 41(2): 29-38. (in Chinese)

    [13] D W ROBINSON, R S MCCLELLAND. Mechanical overview of the international X-ray observatory. MT, 1-10(2009).

    [14] C BEKER, AE TURGUT et al. Design of a novel foldable flapping wing micro air vehicle, 138(2017).

    [15] [15] 15于红英, 许栋铭, 吕学庚. 太阳翼基板的构型分析[J]. 哈尔滨工业大学学报, 2016, 48(1): 46-52. doi: 10.11918/j.issn.0367-6234.2016.01.007YUH Y, XUD M, LÜX G. Configuration analysis of solar wing panels[J]. Journal of Harbin Institute of Technology, 2016, 48(1): 46-52. (in Chinese). doi: 10.11918/j.issn.0367-6234.2016.01.007

    [16] [16] 16高明星. 空间大口径光学主镜展开机构设计[D]. 哈尔滨: 哈尔滨工业大学, 2016. doi: 10.47472/nwjj5082GAOM X. The Design of Deployable Mechanisms of Space Large Aperture Optical Primary Mirror[D]. Harbin: Harbin Institute of Technology, 2016. (in Chinese). doi: 10.47472/nwjj5082

    [17] K MIURA. Method of packaging and deployment of large membranes in space. The Institute of Space and Astronautical Science Report, 618, 1-9(1985).

    [18] Y YOSHIMURA. On the mechanism of buckling of a circular cylindrical shell under axial compression and bending(1951).

    [19] [19] 19黄文宣, 邱慧, 刘峰, 等. 深空探测器防热承力一体化大底结构研究[J]. 航天返回与遥感, 2019, 40(6): 19-25.HUANGW X, QIUH, LIUF, et al. Research on thermal-structural integrated heatshield structure for deep space explorer[J]. Spacecraft Recovery & Remote Sensing, 2019, 40(6): 19-25. (in Chinese)

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    Hong XIAO, Hong-yang WANG, Hong-wei GUO, Sai ZHANG, Rong-qiang LIU, Bin FAN, Jiang BIAN. Design and analysis of the repeatable development and collapse mechanism film protective cover of space camera[J]. Optics and Precision Engineering, 2021, 29(12): 2877

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    Paper Information

    Category: Micro/Nano Technology and Fine Mechanics

    Received: May. 10, 2021

    Accepted: --

    Published Online: Jan. 20, 2022

    The Author Email: GUO Hong-wei (guohw@hit.edu.cn)

    DOI:10.37188/OPE.20212912.2877

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