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文中介绍一种卫星太阳电池阵基板的研究成果。制品选用了碳/环氧面板一蜂窝夹层结构复合材料,可显著减轻结构重量和提高制品的刚度和稳定性。研究成果已应用于实际产品中,取得令人满意的结果。
This article describes a satellite solar array substrate research results. Products selected carbon / epoxy panel honeycomb sandwich composite structure, can significantly reduce the weight of the structure and improve product rigidity and stability. Research results have been applied to the actual product, and achieved satisfactory results.