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首页> 外文期刊>Applied optics >Cryogenic optical measurements of 12-segment-bonded carbon-fiber-reinforced silicon carbide composite mirror with support mechanism
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Cryogenic optical measurements of 12-segment-bonded carbon-fiber-reinforced silicon carbide composite mirror with support mechanism

机译:具有支撑机构的12段键合碳纤维增强碳化硅复合镜的低温光学测量

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摘要

A 720 mm. diameter 12-segment-bonded carbon-fiber-reinforced silicon carbide (C/SiC) composite mirror has been fabricated and tested at cryogenic temperatures. Interferometric measurements show significant cryogenic deformation of the C/SiC composite mirror, which is well reproduced by a model analysis with measured properties of the bonded segments. It is concluded that the deformation is due mostly to variation in coefficients of thermal expansion among segments. In parallel, a 4-degree-of-freedom ball-bearing support mechanism has been developed for cryogenic applications. The C/SiC composite mirror was mounted on an aluminum base plate with the support mechanism and tested again. Cryogenic deformation of the mirror attributed to thermal contraction of the aluminum base plate via the support mechanism is highly reduced by the support, confirming that the newly developed support mechanism is promising for its future application to large-aperture cooled space telescopes. (c) 2008 Optical Society of America.
机译:720毫米直径为12段的碳纤维增强碳化硅(C / SiC)复合镜已制成,并在低温下进行了测试。干涉测量显示C / SiC复合镜的显着低温变形,通过对键合段的测量特性进行模型分析可以很好地再现这种变形。结论是,变形主要是由于段之间的热膨胀系数变化引起的。同时,针对低温应用开发了4自由度滚珠轴承支撑机构。使用支撑机构将C / SiC复合镜安装在铝基板上,并再次进行测试。通过支撑件,可大大减少由于支撑件引起的铝基板热收缩而引起的反射镜的低温变形,这证实了新开发的支撑件有希望将其应用于大口径冷却空间望远镜。 (c)2008年美国眼镜学会。

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