Optics and Precision Engineering, Volume. 23, Issue 11, 3083(2015)

Lightweight design of primary force-taking structures for spacecrafts

LIU Yuan1,*... XIAO Ren-qin2, HAN De-dong3 and GUO Hui-rong2 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(13)

    [2] [2] LIU L, GAO M H. Support technique of deployable unit mirror in space large aperture telescope[J]. Opt. Precision Eng., 2005, 13(3): 127-134. (in Chinese)

    [4] [4] YAO J, TAN SH F, LI M ZH, et al.. Study on the combined and light satellite cylinder[J].Spacecraft Recovery & Remote Sensing, 2010(1): 55-63. (in Chinese)

    [5] [5] LIU X Y. Design and simulation of the composite upstage of aerospace vehicle[D]. Harbin: Harbin Institute of Technology, 2010. (in Chinese)

    [6] [6] MCCARTHY M A, MCCARTHY C T, PADHI G S. A simple method for determining the effects of bolt-hole clearance on load distribution in single-column multi-bolt composite joints[J]. Composite Structures, 2006, 73(1): 78-87.

    [7] [7] WANG W. Optimum Design of Composite Payload Bearing Structure on the Launch Vehicle Acceleration Stage [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010.(in Chinese)

    [13] [13] SUI Y K, ZHANG ZH, DU J ZH. Two-level optimization for section and shape of framed structures[J].Engineering Mechanics, 2009, 26(8): 116-122. (in Chinese)

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    LIU Yuan, XIAO Ren-qin, HAN De-dong, GUO Hui-rong. Lightweight design of primary force-taking structures for spacecrafts[J]. Optics and Precision Engineering, 2015, 23(11): 3083

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    Paper Information

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    Received: Jun. 10, 2015

    Accepted: --

    Published Online: Jan. 25, 2016

    The Author Email: Yuan LIU (liuyuan_hit@hit.edu.cn)

    DOI:10.3788/ope.20152311.3083

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