| 固体火箭发动机粘接界面湿热老化特性探究 |
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| 引用本文： | 王斌. 固体火箭发动机粘接界面湿热老化特性探究[J]. 中国胶粘剂, 2006, 15(7): 5-7 |
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| 作者姓名： | 王斌 |
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| 作者单位： | 中国人民解放军第二炮兵工程学院 陕西省西安市 |
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| 摘 要： | 对常用的加速老化寿命模型进行了归纳、总结,在分析其原理的基础上,针对固体火箭发动机粘接界面在湿热环境下的失效机理,提出合适的湿热老化寿命模型,可作为固体火箭发动机粘接界面湿热环境适应性研究的理论依据。
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| 关 键 词： | 固体火箭发动机 粘接界面 湿热老化 环境适应性 |
| 文章编号： | 1004-2849(2006)07-0005-03 |
| 收稿时间： | 2006-02-24 |
| 修稿时间： | 2006-03-01 |
Research to the hygrothermal ageing characteristic of solid rocket motor(SRM) adhint |
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| WANG Bin. Research to the hygrothermal ageing characteristic of solid rocket motor(SRM) adhint[J]. China Adhesives, 2006, 15(7): 5-7 |
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| Authors: | WANG Bin |
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| Abstract: | This paper summed up the accelerated ageing life models in common use, and, by studying the homologous principles, advanced appropriate hygrothermal ageing life model corresponding to the abating mechanism of SRM adhesive joint in hygrothermal environment. The model can be used as a theoretic gist in studying the hygrothermal environment adaptability of SRM adhint |
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| Keywords: | SRM(solid rocket motor) adhint hygrothermal ageing environment adaptability |
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