| 航天器复合材料胶接连接工艺分析 |
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| 引用本文： | 沃西源,涂彬,夏英伟.航天器复合材料胶接连接工艺分析[J].航天返回与遥感,2008,29(4):62-66. |
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| 作者姓名： | 沃西源 涂彬 夏英伟 |
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| 作者单位： | 北京空间机电研究所,北京,100076 |
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| 摘 要： | 文章叙述了航天器复合材料胶接工艺应具备的条件，航天器产品常用胶粘剂及其特性，研制航天器复合材料耐久型胶接结构基本要素及复合材料胶接连接工艺特性和品质控制等内容。
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| 关 键 词： | 胶接连接 品质控制 复合材料 航天器 |
Analysis of Adhesive Technology in Spacecraft Composite Materials |
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| Wo Xiyuan,Tu bin,Xia Yingwei.Analysis of Adhesive Technology in Spacecraft Composite Materials[J].Spacecraft Recovery & Remote Sensing,2008,29(4):62-66. |
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| Authors: | Wo Xiyuan Tu bin Xia Yingwei |
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| Abstract: | This article introduced the conditions which should be provided in the adhesive technology of spacecraft composite materials and the properties of the typical adhesives.Also the basic element of durable adhesive structure,characteristics of the adhesive technology and quality control were mentioned in the paper. |
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| Keywords: | Adhesive joint Quality control Composite material Spacecraft |
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