Infrared and Laser Engineering, Volume. 52, Issue 5, 20220742(2023)

Low thermal expansion optimization of composite support structure for missile-borne optical system

Xuan Wang and Chenqi Zhao
Author Affiliations
  • College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China
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    References(13)

    [4] M N Velea, S Lache. Thermal expansion of composite laminates Bulletin of the Transilvania University of Brasov. Engineering Sciences. Series I, 8, 25(2015).

    [7] [7] Song Weiyang. A design of CFRP suppted structure f a new space camera research on mechanical thermal stability of the camera [D]. Changchun: Changchun Institute of Optics, Fine Mechanics Physics, Chinese Academy of Sciences (University of Chinese Academy of Sciences), 2022. (in Chinese)

    [9] Xueqiong Qiu, Lin Chen. Test and theoretical method for coefficients of thermal expansion of carbon fiber reinforced composite laminate. Composites Science and Engineering, 28-32, 104(2021).

    [10] [10] ASTM International. Stard test method f linear thermal expansion of solid materials by thermomechanical analysis: ASTM E83119[S]. United States: ASTM International, West Conshohocken, PA, 2014.

    [13] Jianke Zhang. Thermal expansion——One of thermophysical properties of carbon fiber/epoxy-resin composites. Chinese Space Science and Technology, 45-50, 69(1987).

    [16] Liang He, Panxing Zhu, Xiaowei Xu, . A review on mechanism and control methods of residual stress and cured deformation of composite materials. Composite Materials and Engineering, 121-128(2022).

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    Xuan Wang, Chenqi Zhao. Low thermal expansion optimization of composite support structure for missile-borne optical system[J]. Infrared and Laser Engineering, 2023, 52(5): 20220742

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    Paper Information

    Category: Material & Thim films

    Received: Oct. 25, 2022

    Accepted: --

    Published Online: Jul. 4, 2023

    The Author Email:

    DOI:10.3788/IRLA20220742

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