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利用空间综合辐照地面模拟试验装置和热重分析、XPS分析等对空间近紫外辐射环境下均苯型聚酰亚胺(PI)薄膜力学性能演化的数学模型和物理模型进行了研究。研究发现,均苯型PI 薄膜抗拉强度和断裂伸长率随着近紫外曝辐量的增加先降低而后呈现指数增加,最后趋于稳定。由热重分析和 XPS 分析可知,在近紫外辐照初期,C—O、C—C、C—N等价键的断裂是的导致其力学性能降低的主要原因,而后随着近紫外曝辐量的增加,不同分子链之间的交联是PI薄膜力学性能增加的主要原因。

The mechanical property and mechanism of polyimide film in near ultraviolet was studied and follow-ing results can be obtained:with the increasing of near ultraviolet,the rupture elongation and tensile strength of polyimide decrease firstly and then exponentially increase utile to stable.The breakage and cross linkage of molecular bond is the maj or cause of change of polyimide’s mechanical property in ultraviolet environments, and breakage of C—O,C—C,C—N is the major origin in early stage of irradiation and cross linkage is for the increase of mechanical property in subsequent ultraviolet irradiation.

参考文献

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[2] Tesia L. Albarado;William A. Hollerman;David Edwards;Whitney Hubbs;Charles Semmel.Electron Exposure Measurements of Candidate Solar Sail Materials[J].Journal of Solar Energy Engineering,20051(1):125-130.
[3] 沈自才;郑慧奇;赵雪;冯伟泉;刘宇明;赵春晴;丁义刚.远紫外辐射下Kapton/Al薄膜材料的力学性能研究[J].航天器环境工程,2010(5):600-603.
[4] 张帆;沈自才;冯伟泉;郑慧奇;丁义刚;赵春晴.均苯型聚酰亚胺薄膜在质子辐照下的力学性能退化试验研究[J].航天器环境工程,2012(3):315-319.
[5] 黄小琦;王立;刘宇飞;高鸿;王永建;田海;冯展祖;柳青.太阳帆表面薄膜空间电子辐照性能研究[J].真空与低温,2014(3):154-157.
[6] 徐坚;杨斌;杨猛;蔡震波.空间紫外辐照对高分子材料破坏机理研究综述[J].航天器环境工程,2011(1):25-30.
[7] 沈自才;李衍存;丁义刚.航天材料紫外辐射效应地面模拟试验方法[J].航天器环境工程,2015(1):43-48.
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