摘要
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 paper introduces a solar array substrate for the satellite utilized carbon/ epoxy facing - honeycomb sandwich composites. The structures weight is obviously reduced, rigidity and stability are improved. The product has successfully used in practice.
出处
《航天返回与遥感》
1996年第4期43-49,共7页
Spacecraft Recovery & Remote Sensing
