Volume 41 Issue 1
Mar.  2012
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Dong Deping, Zhang Yulin, Lu Yan. Application of radiant coolers on Chinese meteorological satellites[J]. Infrared and Laser Engineering, 2012, 41(1): 119-123.
Citation: Dong Deping, Zhang Yulin, Lu Yan. Application of radiant coolers on Chinese meteorological satellites[J]. Infrared and Laser Engineering, 2012, 41(1): 119-123.

Application of radiant coolers on Chinese meteorological satellites

  • Publish Date: 2012-01-25
  • Optical remote sensing instruments including IR detection channels are always the major payloads of meteorological satellites. Radiant coolers are used for cooling the IR detectors and its aft optics to the desired temperatures, aboard on Chinese polar orbit meteorological satellites and geostationary orbit meteorological satellites. Depending on the requirements of optical instruments and satellites on the radiant coolers, the different style coolers such as W style, O style, L style, G style and octahedron-cone style in the past 30 years were studied, and the flight performance of the radiant coolers on FY-1A to FY-1D, FY-3A/ 3B, FY-2A to FY-2E meteorological satellites were presented. The lowest temperature of radiant cooler on FY-3 satellite was about 85 K and had 120 mW at 100 K. The concerned technologies needed for long-life operational meteorological satellites were discussed and its application results were also given. The possible application of passive cooling technology in future was discussed.
  • [1] Gong Haimei, Liu Dafu. Developments and trends in spaceborne infrared detectors[J]. Infrared and Laser Engineering, 2008, 37(1): 18-24. (in Chinese).
    [2]
    [3] Li Qing, Dong Yaohai. Developments of Chinese meteorological satellites[J]. Shanghai Aerospace, 2008(1): 1-8. (in Chinese).
    [4] 龚海梅, 刘大福. 航天红外探测器的发展现状与进展[J]. 红外与激光工程, 2008, 37(1): 18-24.
    [5] Dong Yaohai, Sun Yunzhu, Wang Jinhua, et al. FY-3A polar orbit meteorological satellite[J]. Shanghai Aerospace, 2008(5): 1-11. (in Chinese)
    [6]
    [7] Zhang Yulin, Zhou Xiyang. Performance of FY-2(02) radiant coolers in orbits[J]. Cryogenics and Superconductors, 2009(S): 200-204. (in Chinese)
    [8]
    [9] Dong Deping, Wang Weiyang. Study of cryodeposition contamination of radiant coolers[C]// Proceedings of 16 th ICEC/ ICMC, 1996: 719-722.
    [10] 李卿, 董瑶海. 中国气象卫星技术成就与展望[J]. 上海航天, 2008(1): 1-8.
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    [13] 董瑶海, 孙允珠, 王金华, 等. FY-3A极轨气象卫星[J]. 上海航天, 2008(5): 1-11.
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    [16] 张玉林, 周夕言. 风云二号02批辐射制冷器在轨情况[J]. 低温与超导, 2009(S): 200-204.
    [17]
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Application of radiant coolers on Chinese meteorological satellites

  • 1. Shanghai Institute of Technical Physics,Chinese Academy of Sciences,Shanghai 200083,China

Abstract: Optical remote sensing instruments including IR detection channels are always the major payloads of meteorological satellites. Radiant coolers are used for cooling the IR detectors and its aft optics to the desired temperatures, aboard on Chinese polar orbit meteorological satellites and geostationary orbit meteorological satellites. Depending on the requirements of optical instruments and satellites on the radiant coolers, the different style coolers such as W style, O style, L style, G style and octahedron-cone style in the past 30 years were studied, and the flight performance of the radiant coolers on FY-1A to FY-1D, FY-3A/ 3B, FY-2A to FY-2E meteorological satellites were presented. The lowest temperature of radiant cooler on FY-3 satellite was about 85 K and had 120 mW at 100 K. The concerned technologies needed for long-life operational meteorological satellites were discussed and its application results were also given. The possible application of passive cooling technology in future was discussed.

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