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Low-temperature figure stability of a COI all-composite mirror M4

机译:COI全复合镜M4的低温图形稳定性

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Abstract: Recent developments in the design and fabrication of very light-weight all-composite mirrors have made possible extremely well balanced, thermally stable, structures which distort very little when cooled. One such mirror is the Composite Optics, Incorporated all-composite mirror, M4, which has a 45.7 cm diameter and 3 cm thickness and a spherical surface of radius-of-curvature 2.92 meters. Relative figure measurements of this mirror were made with the Steward Observatory Light Weight Mirror Low Temperature Test Chamber over a temperature range from 20 C to $MIN@60 C using a 10.6 micrometer interferometer. The measurements show a remarkably small increase in the rms figure departure from a spherical surface of fixed radius-of-curvature of 0.27 micrometer over the 80 C temperature change. The effective coefficient of thermal expansion over this temperature range derived from the focus change is 0.66 $MUL 10$+$MIN@6$//C, close to that of fused silica. !4
机译:摘要:非常轻巧的全复合镜的设计和制造方面的最新发展,使得非常平衡,热稳定,冷却时变形很小的结构成为可能。一种这样的镜子是Composite Optics,Incorporated全复合镜子M4,其直径为45.7cm,厚度为3cm,并且球面的曲率半径为2.92米。该镜子的相对图形测量是使用Steward天文台轻型镜子低温测试箱在10.6微米干涉仪上在20 C至MIN @ 60 C的温度范围内进行的。测量结果表明,在80 C温度变化下,均方根值与固定曲率半径为0.27微米的球面的均方根值的增加非常小。由焦点变化得出的在此温度范围内的有效热膨胀系数为0.66 $ MUL 10 $ + $ MIN @ 6 $ // C,接近熔融二氧化硅。 !4

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