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Design, fabrication and testing of active carbon shell mirrors for space telescope applications

机译:用于太空望远镜应用的活性碳壳镜的设计,制造和测试

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摘要

A novel active mirror concept based on carbon fiber reinforced polymer (CFRP) materials is presented. A nanolaminate facesheet, active piezoelectric layer and printed electronics are implemented in order to provide the reflective surface, actuation capabilities and electrical wiring for the mirror. Mirrors of this design are extremely thin (500-850 µm), lightweight (~ 2 kg/m^2) and have large actuation capabilities (~ 100 µm peak- to-valley deformation per channel). Replication techniques along with simple bonding/transferring processes are implemented eliminating the need for grinding and polishing steps. An outline of the overall design, component materials and fabrication processes is presented. A method to size the active layer for a given mirror design, along with simulation predictions on the correction capabilities of the mirror are also outlined. A custom metrology system used to capture the highly deformable nature of the mirrors is demonstrated along with preliminary prototype measurements.
机译:提出了一种基于碳纤维增强聚合物(CFRP)材料的新型主动镜概念。实施纳米层压面板,有源压电层和印刷电子器件,以提供反射镜的反射表面,驱动能力和电线。这种设计的反射镜非常薄(500-850 µm),重量轻(〜2 kg / m ^ 2)并且具有很大的驱动能力(每个通道的峰谷变形约为100 µm)。复制技术以及简单的键合/转移过程得以实现,从而无需进行研磨和抛光步骤。介绍了总体设计,组件材料和制造过程的概述。还概述了一种用于给定反射镜设计的有源层尺寸的方法,以及关于反射镜校正功能的仿真预测。演示了用于捕获反射镜高度易变形性质的定制度量系统以及初步的原型测量。

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