空间充气展开结构用刚化材料和刚化技术的研究现状

材料工程, 2008, (2): 76-80. doi: 10.3969/j.issn.1001-4381.2008.02.018

空间充气展开结构用刚化材料和刚化技术的研究现状

刘宇艳 ^1, , 孟秋影 ^2, , 谭惠丰 ^3, , 杜星文 ^4,

1.哈尔滨工业大学,哈尔滨,150001

2.哈尔滨工业大学,哈尔滨,150001

3.哈尔滨工业大学,哈尔滨,150001

4.哈尔滨工业大学,哈尔滨,150001

基金项目: 哈尔滨工业大学校科研和教改项目(HIT.2006.32)

关键词：空间充气展开结构 , 刚化材料 , 刚化技术

The Situation of the Rigidizable Materials and Rigidization Technology Used in Space Inflatable Structures

刚化技术和刚化材料是空间充气展开结构的一项合材料;热塑性(和轻度交联热固性)复合材料;铝/聚合物层合板.本文介绍了这几种材料的典型刚化技术,分别介绍了刚化体系的特点、研究现状以及该刚化技术相应的优势与局限性.

参考文献

[1]	FREELAND R E;BILYEU G D;VEAL G R.Inflatable deployable space structures technology summart[A].Melbourne:International Astronautical Federation,1998:1-10.
[2]	DAROOKA D K;JENSEN D W.Advanced space structure concepts and their development[A].Seattle:American Institute of Aeronautics and Astronautics,2001:1-10.
[3]	FREELAND R;BILYEN G.In-step inflatable antenna experiment[A].Washington:International Astronautical Federation,1992:1-16.
[4]	BILLY D.Case studies in inflatable rigidizable structural concepts for space power[A].Missouri:American Institute of Aeronautics and Astronautics,1999:58-74.
[5]	HIROAKI T;YUMI S.Rigidizable membranes for apace inflatable structures[A].Denver;American Institute of Aeronautics and Astronautics,2002:1-7.
[6]	ALLRED R E;HOYT A E;MCELROY P M.UV rigidizable carbon-reinforced isogrid inflatable booms[A].Denver:American Institute of Aeronautics and Astronautics,2002:1-11.
[7]	SIMBURGER E J;GIANTS T W;MATSUMOTO J H.Development,design,and testing of power sphere muhifunctional ultraviolet-rigidizable inflatable structures[A].Norfolk:American Institute of Aeronautics and Astronautics,2003:1-11.
[8]	ALLRED R;HARRAH L;MCELROY P.Inflatable spacecraft using rigidization on command concept[A].Atlanta:American Institute of Aeronautics and Astronautics,2000:1-11.
[9]	FREELAND R E;VEAL G R.Significance of the inflatable antenna experiment technology[A].California:American Institute of Aeronautics and Astronautics,1998:1-16.
[10]	GUIDANEAN K;LICHODZIEJEWSKI D.An inflatable rigidizable truss structure based on new sub-Tg polyurethane composites[A].Denver:American Institute of Aeronautics and Astronautics,2002:1-11.
[11]	CADOGAN D P;SCARBOROUGH S E.Shape Memory Composite Development for Use in Gossamer Space Inflatable Structures[A].Denver:American Institute of Aeronautics and Astronautics,2002:1-12.
[12]	MARC R S;WILLIAM H F;DOUGLAS C.Analysis techniques for shape-memory composite structures[A].Hawaii:American Institute of Aeronautics and Astronautics,2007:1-11.
[13]	CADOGAN D P;SCARBOROUGH S E.Rigidizable materials for use in gossamer space inflatable structures[A].Seattle:American Institute of Aeronautics and Astronautics,2001:1-14.
[14]	SCHNELL A R;LEIGH L M;TINKER M L.Deployment,foam rigidization,and structural characterization of inflatable thin-film booms[A].Denver:American Institute of Aeronautics and Astronautics,2002:1-7.
[15]	GUIDANEAN K;VEAL G.An inflatable rigidizable calibration optical sphere[A].Norfolk:American Institute of Aeronautics and Astronautics,2003:1-9.
[16]	LICHODZIEJEWSKI D;VEAL G;DERB S B.Spiral wrapped aluminum laminate rigidization technology[A].Denver:American Institute of Aeronautics and Astronautics,2002:1-8.

上一张下一张

上一张下一张

计量

下载量()
访问量()

作者相关

文章评分

您的评分：
1

0%
2

0%
3

0%
4

0%
5

0%