名称:卫星轻量化支架 材料:AIsi10Mg 应用场景:某型号卫星 产品状态:试制件 技术指标:最大位移<0.2mm,最大应力<30Mpa,基频<1500HZ,重量976g 技术特点:某型号卫星太阳电池阵驱动机构安装支架经过拓扑优化后,重量降低幅度达到74%。
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