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航天器热控材料的应用和发展 被引量:16

Spacecraft Thermal Control Materials
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摘要 文摘介绍了航天器热控系统对材料的要求以及应用的情况,并根据航天器总体和热控技术的需求,对热控材料的发展提出初步的建议。 There is an introduction to the requirements and applications for thermal control material in this paper. Future material development tendencies faced with spacecraft system and thermal control technologies are put forward.
作者 范含林
出处 《宇航材料工艺》 CAS CSCD 北大核心 2007年第6期7-10,共4页 Aerospace Materials & Technology
关键词 航天器 热控材料 发展 应用 隔热材料 表面涂层材料 Spacecraft, Thermal control, Material
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参考文献9

  • 1何知朱,江经善.新型热控材料器件及应用.北京:中国宇航出版社,1988.
  • 2范庆梅等.大型通信卫星天线敏感性的热分析验证.见:第七届空间热物理会议文集,2005.
  • 3Birur G C, Stultz J W, Tsuyki G T. Novel lightweight thermal insulation type for martian environment: using carbon dioxide gas and aerogel in hghtweight thermal enclosures. In: 11th Annual spacecraft thermal control technology workshop. The Aerospace Corporation, EI Segundo, CA, 2000.
  • 4Swanson T D, Birur G C. NASA thermal control technologies for robtic spacecraft: In: Paper for the 12th IHPC-April 4, 2002.
  • 5Chandrasekhar P. Conducting polymer based actively IR modulating electrochromics for varied spacecraft application. In: 10th annual spacecraft thermal control technology workshop. The Aerospace Corporation, LA, 1999.
  • 6Ann Garrison Darrin et al. Variable emissivity through MEMS technology. CP458, Space Technology and Applications Inter. Forum-2000.
  • 7Donya M D, Theodore S, Robert O et al. Development of the variable emittance thermal suite for the space technology 5 microsatellite. STIAF, 2002.
  • 8林来兴.ST-5微小卫星与星座及其空间飞行验证——为未来微小卫星的空间应用展现广阔前景[J].航天器工程,2007,16(1):63-68. 被引量:6
  • 9Lisa M,Theodore D S. Parametric study of variable emissivity radiator surface. STAIF, 2000.

二级参考文献2

  • 1Candace C,Carlisle E J,Finnegan.Space Technology-5pa-thfinder for future micro-sat constellation[].IEEE Aerospace confproc.2004
  • 2Candace C,Carlisle E H,et al.Space Technology-5chang-ing the mission design without changing the hardware[]..2005

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引证文献16

二级引证文献58

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