期刊文献+

航天器可展开支撑杆的研制及其收拢展开特性研究 被引量:9

Fabrication and Retraction/Deployment Testings of Space Deployable Booms
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摘要 复合材料豆荚杆是一种质量轻、刚度较大、收拢效率高、展开过程可靠的可展开管状杆结构。本工作对豆荚杆进行优化设计,并对多种豆荚杆试件进行性能测试与评估,选取其中综合性能优异的材料体系研制了2m长豆荚杆样机。利用研制的豆荚杆收展控制机构对豆荚杆的收拢-展开性能进行了测试,结果显示玻璃布/FEB豆荚杆可实现多次收拢-展开,其综合性能可基本满足空间可展开结构的性能需求。 The pod-shape-crossection boom is a kind of storable tubular extendible member with excellent stiffness-to-weight ratio,stowed ratio and deployment reliability.A series of pod-shape-crossection boom samples are prepared and tested.The results suggest that Fiberglass/FEG composite has preferable properties in fabricating pod-shape-crossection booms.A 2m-long boom prototype based on selected Fiberglass/FEG composite is manufactured,retraction/deployment testings are conducted.Results implies that the obtained booms are applicable for space missions.
出处 《材料工程》 EI CAS CSCD 北大核心 2009年第S2期157-160,共4页 Journal of Materials Engineering
基金 上海市重点实验室项目(06DZ22105) 上海市科委科技专项项目(09DZ1110300)
关键词 可展开结构 豆荚杆 收拢展开特性 space deployable structure pod boom retraction/deployment testing
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参考文献3

  • 1F Rehnmark,,MPryor,B Hol mes,et al.Development of a De-ployable Nonmetallic Boomfor Reconfigurable Systems of Small Spacecraft. AI AA2007-2184 .
  • 2MLeipold,HRunge,C Sickinger.Large SAR Membrane Anten-nas with Lightweight Deployable Booms. AI AA2007-2184 .
  • 3Christoph Sickinger Lars Herbeck and Elmar Breitbach.Structural engineering on deployable CFRP booms for a solar propelled sailcraft[].Acta Astronautica.2006

同被引文献48

  • 1马兴瑞,于登云,孙京,胡成威.空间飞行器展开与驱动机构研究进展[J].宇航学报,2006,27(6):1123-1131. 被引量:59
  • 2杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1025
  • 3陈烈民,沃西源.航天器结构材料的应用和发展[J].航天返回与遥感,2007,28(1):58-61. 被引量:20
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  • 8李瑞祥,唐国金,咸奎成,等.空间豆荚杆伸展机构设计与力学分析[C].中国空间科学学会空间机电与空间光学专业委员会2010年学术交流会,合肥,2010年8月28-30日.
  • 9Leipold M, Runge H, Sickingcr C. Large SAR membrane antennas with light weight deployable booms[ C ]. 28th ESA Antenna Workshop on Space Antenna Systems and Technologies, ESA/ ESTEC, Noordwijk, Netherlands, May 31 - June 3, 2005.
  • 10Sickinger C, Herbeck L, Breitbach E. Structural engineering on deployable CFRP booms for a solar propelled sailcraft[ J]. Acta Astronautica, 2006(58) : 185 - 196.

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