Infrared and Laser Engineering, Volume. 52, Issue 11, 20230257(2023)

Design for eliminating radiant heat difference of focal surface window in spaceborne remote sensing camera

Yongkun Li1, Changchun Gao1, Jianchao Jiao1, Limin Wu1, and Zhentao Yu2
Author Affiliations
  • 1Beijing Institute of Mechanics & Electricity, Beijing 100094, China
  • 2Navy Submarine Acadmy, Qingdao 266000, China
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    Figures & Tables(9)
    Composition of camera
    Optical system imaging model
    Contrastive MTF of lens
    Light blocking window design
    Finite element model of thermal simulation of whole camera
    Comparative temperature simulation diagram of mirror 8
    Improved temperature curve of mirror 8
    Simulation results of themal deformation of mirror and improved MTF of lens
    • Table 1. Material parameters of each component

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      Table 1. Material parameters of each component

      MaterialApplication partDensity/kg·m–3Conductivity/W·m–1·K–1Expansion (10−6)/K
      AluminiumFocal box/Cone2700117.210.73
      7980Blocking window22001.380.51
      TC4Lens bracket444015.210.2
      H-LAF50BMirror 44240-5.8
      H-ZLAF52AMirror 5, 74480-6.1
      H-FK61Mirror 2, 3, 83700-13.1
      H-LAF3BMirror 1, 64500-8
      D263TFocal window2510-7.2
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    Yongkun Li, Changchun Gao, Jianchao Jiao, Limin Wu, Zhentao Yu. Design for eliminating radiant heat difference of focal surface window in spaceborne remote sensing camera[J]. Infrared and Laser Engineering, 2023, 52(11): 20230257

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    Paper Information

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    Received: Apr. 26, 2023

    Accepted: --

    Published Online: Jan. 8, 2024

    The Author Email:

    DOI:10.3788/IRLA20230257

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