Volume 43 Issue S1
Jan.  2015
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Kong Lin. A review of thermal control subsystem design methods and key technologies for small speedy responsive space satellites[J]. Infrared and Laser Engineering, 2014, 43(S1): 130-138.
Citation: Kong Lin. A review of thermal control subsystem design methods and key technologies for small speedy responsive space satellites[J]. Infrared and Laser Engineering, 2014, 43(S1): 130-138.

A review of thermal control subsystem design methods and key technologies for small speedy responsive space satellites

  • Received Date: 2014-10-10
  • Rev Recd Date: 2014-11-09
  • Publish Date: 2015-01-25
  • With the development of space technology, satellite thermal control systems face new challenges. First, a detailed comparison of traditional and responsive thermal control systems was presented according to the characters of small speedy responsive space satellites, and then a new design process was derived for responsive thermal control systems. Each of the key technologies including a single hot and cold case design orbits, modular thermal architectures, fast analysis and virtual test method was introduced. Finally, the advanced equipment and materials for responsive thermal control were reviewed. In a word, the author considers that a robust modular scalable thermal control with new advanced smart thermal control device was the certain requirement and way to implement responsive thermal control systems.
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    [3] Williams A D, M Eric Lyall, Derek W Hengeveld, et al. Thermal control subsystem requirements and challenges for a responsive satellite bus[C] //SPIE, 7330: 154-161.
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    [19] Dou Qiang, Pang Hewei, Wei Chuanfeng, et al. The software architecture spacecraft virtual platform and its application[J]. Spacecraft Environment Engineering, 2007, 24(6): 370-373. (in Chinese) 窦强, 庞贺伟, 魏传峰, 等. 航天器虚拟热试验平台的软件架构及其应用[J]. 航天器环境工程, 2007, 24(6): 370-373.
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    [27] Liu Dongqing, Chen Haifeng, Zheng Wenwei, et al. Application of variable infrared-emissivity materials to spacecraft thermal control[J]. Journal of National University of Defense Technology, 2012, 34(2): 145-149. (in Chinese) 刘东青, 程海峰, 郑文伟, 等. 红外发射率可变材料在航天器热控技术中的应用 [J]. 国防科技大学学报, 2012, 34(2): 145-149.
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A review of thermal control subsystem design methods and key technologies for small speedy responsive space satellites

  • 1. National & Local United Engineering Research Center of Small Satellite Technology,Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China

Abstract: With the development of space technology, satellite thermal control systems face new challenges. First, a detailed comparison of traditional and responsive thermal control systems was presented according to the characters of small speedy responsive space satellites, and then a new design process was derived for responsive thermal control systems. Each of the key technologies including a single hot and cold case design orbits, modular thermal architectures, fast analysis and virtual test method was introduced. Finally, the advanced equipment and materials for responsive thermal control were reviewed. In a word, the author considers that a robust modular scalable thermal control with new advanced smart thermal control device was the certain requirement and way to implement responsive thermal control systems.

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