Optical Instruments, Volume. 37, Issue 2, 116(2015)

Verification of thermal design and in-orbit flight for large off-axis triple-mirror anastigmatic camera

CHEN Weichun1、* and WANG Haixing2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    References(4)

    [2] [2] GILMORE D G.Spacecraft thermal control handbook: fundamental technologies[M].Galifornia: The Aerospace Press,2002: 21-36.

    [6] [6] STOECKEL G,CROMPTON D,PERRON G.Advancements in integrated structural/thermal/optical(STOP)analysis of optical systems[J].SPIE,2007,6675: 66750D1-66750D14.

    [7] [7] JOHNSON G B.Thermal management for CCD performance on the advanced camera for surveys(ACS)[J].SPIE,1998,3356: 284-291.

    [10] [10] XIN H W,LI Z L.Structural design for lightweight off-axis TMA space telescope[C]∥2011 Second International Conference on Digital Manufacturing and Automation.Zhangjiajie: IEEE,2011: 1125-1128.

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    CHEN Weichun, WANG Haixing. Verification of thermal design and in-orbit flight for large off-axis triple-mirror anastigmatic camera[J]. Optical Instruments, 2015, 37(2): 116

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    Paper Information

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    Received: Jun. 27, 2014

    Accepted: --

    Published Online: May. 20, 2015

    The Author Email: CHEN Weichun (chenweichun111@sina.cn)

    DOI:10.3969/j.issn.1005-5630.2015.02.006

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