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太阳帆材料研究进展 被引量:2

Recent Progress on Solar Sail Materials
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摘要 太阳帆飞船由于无需动力等优势近年来引起了各国科学家的研究兴趣,并在深空探测领域具有重要的应用前景。太阳帆的结构设计和材料选择是影响其性能的重要因素,本文结合太阳帆飞行环境的特点,介绍了太阳帆的基本结构和飞行原理,重点针对目前几种比较典型的太阳帆设计,对其支撑材料以及帆面薄膜材料进行了综述,并分析了各种材料和设计的性能特点。 Non-powered solar sails are arousing more and more research interest all over the world in recent years, which have significant potential applications in deep-space exploration due to their unique advantages. The structures and materials are critical factors for solar sails. According to the flight environment of solar sails, this paper introduced their basic structures and mechanisms, and reviewed the deployable boom materials and sail membrane materials for some typical solar sail designs. The features of different materials and designs were also discussed.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2013年第4期24-28,共5页 Aerospace Materials & Technology
关键词 飞行器 太阳帆 结构 材料 Aircraft, Solar sail, Structure, Materials
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同被引文献19

  • 1陈健,曹永,陈君.太阳帆推进技术研究现状及其关键技术分析[J].火箭推进,2006,32(5):37-42. 被引量:7
  • 2田利思,李相辉,马越峰.MSCNastran动力分析指南[M].北京:中国水利水电出版社,2012(3).
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  • 5WIE B. AOCS performance and stability validation for large, flexible solar sail spacecraft [ R ]. AIAA 2005- 3926, 2005.
  • 6ZHANG J. Coupled attitude-orbit control of flexible so- lar sail for displaced solar orbit [ J]. Journal of Space- craft and Rockets, 2013, 50 (3) :675-685.
  • 7LI Q. Reduced model for flexible solar sail dynamics [J]. Journal of Spacecraft and Rockets, 2011, 48(3) : 446-453.
  • 8SU X F, FRANK A, BARMAC T, et al. Wrinkling analysis of a Kapton square membrane under tensile load- ing [R]. AIAA 2003-1985, 2003.
  • 9尚海滨,崔平远,栾恩杰.近地小推力转移轨道的加权组合制导策略[J].航空学报,2007,28(6):1419-1427. 被引量:4
  • 10王长国,杜星文,赫晓东.空间充气薄膜结构的褶皱分析[J].力学学报,2008,40(3):331-338. 被引量:14

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