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本文从实用角度分析了在航天器复合材料结构胶接成型中所用胶粘剂的选择原则。针对航天器复合材料结构的使用环境,分别从设计要求、耐温性和工艺等方面分析了一些胶粘剂的适用性。
This paper analyzes the selection principle of the adhesive used in the bonding of the spacecraft composite structure from a practical point of view. In view of the use environment of the spacecraft composite structure, the applicability of some adhesives is analyzed respectively from the design requirements, temperature resistance and technology.