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.
参考文献
| [1] | 闵桂荣;郭舜.航天器热控制[M].北京:科学出版社,1998 |
| [2] | 何知朱;江经善.新型热控材料器件及应用[M].北京:宇航出版社,1988 |
| [3] | 范庆梅.大型通信卫星天线敏感性的热分析验证[A].,2005 |
| [4] | Birur G C;Stultz J W;Tsuyki G T.Novel lightweight thermal insulation type for martian environment:using carbon dioxide gas and aerogel in lightweight thermal enclosures[A].The Aerospace Corporation EI Segundo CA,2000 |
| [5] | Swanson T D;Birur G C.NASA thermal control technologies for robtic spacecraft[A].,2002 |
| [6] | Chandrasekhar P.Conducting polymer based actively IR modulating electrochromics for varied spacecraft application[A].The Aerospace Corporation LA,1999 |
| [7] | Ann Garrison Darrin.Variable emissivity through MEMS technology[A]. |
| [8] | Donya M D;Theodore S;Robert O.Development of the variable emittance thermal suite for the space technology 5 microsatellite[M].STIAF,2002 |
| [9] | 林来兴.ST-5 微小卫星及其空间飞行验证--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(01):63-68. |
| [10] | Lisa M;Theodore D S.Parametric study of variable emissivity radiator surface[M].STAIF,2000 |
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