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Lightweight deformable mirrors for future space telescopes.

机译:用于未来太空望远镜的轻型可变形反射镜。

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摘要

This thesis presents a concept for ultra-lightweight deformable mirrors based on a thin substrate of optical surface quality coated with continuous active piezopolymer layers that provide modes of actuation and shape correction. This concept eliminates any kind of stiff backing structure for the mirror surface and exploits micro-fabrication technologies to provide a tight integration of the active materials into the mirror structure, to avoid actuator print-through effects. Proof-of-concept, 10-cm-diameter mirrors with a low areal density of about 0.5 kg/m2 have been designed, built and tested to measure their shape-correction performance and verify the models used for design. The low cost manufacturing scheme uses replication techniques, and strives for minimizing residual stresses that deviate the optical figure from the master mandrel. It does not require precision tolerancing, is lightweight, and is therefore potentially scalable to larger diameters for use in large, modular space telescopes. Other potential applications for such a laminate could include ground-based mirrors for solar energy collection, adaptive optics for atmospheric turbulence, laser communications, and other shape control applications.;The immediate application for these mirrors is for the Autonomous Assembly and Reconfiguration of a Space Telescope (AAReST) mission, which is a university mission under development by Caltech, the University of Surrey, and JPL. The design concept, fabrication methodology, material behaviors and measurements, mirror modeling, mounting and control electronics design, shape control experiments, predictive performance analysis, and remaining challenges are presented herein. The experiments have validated numerical models of the mirror, and the mirror models have been used within a model of the telescope in order to predict the optical performance. A demonstration of this mirror concept, along with other new telescope technologies, is planned to take place during the AAReST mission.
机译:本文提出了一种超轻型可变形镜的概念,该镜基于光学表面质量较薄的基板,并涂有连续的活性压电聚合物层,可提供致动和形状校正模式。该概念消除了镜面的任何种类的刚性背衬结构,并利用微细加工技术将活性材料紧密集成到镜面结构中,从而避免了执行机构的透印效果。已经设计,制造和测试了概念验证的直径为10厘米,面密度为0.5 kg / m2的低反射镜,以测量其形状校正性能并验证用于设计的模型。低成本制造方案使用复制技术,并努力使残余应力最小化,该残余应力使光学图形偏离了主模轴。它不需要精确的公差,重量轻,因此有可能扩展到更大的直径,以用于大型模块化太空望远镜。这种层压板的其他潜在应用可能包括用于太阳能收集的地基反射镜,用于大气湍流的自适应光学器件,激光通信以及其他形状控制应用;这些反射镜的直接应用是空间的自动组装和重新配置。望远镜(AAReST)任务,这是由加州理工学院,萨里大学和JPL开发的大学任务。本文介绍了设计概念,制造方法,材料性能和测量,镜面建模,安装和控制电子设备设计,形状控制实验,预测性能分析以及其他挑战。实验已经验证了镜子的数值模型,并且为了预测光学性能,已经在望远镜的模型中使用了镜子模型。计划在AAReST任务期间对该镜概念以及其他新的望远镜技术进行演示。

著录项

  • 作者

    Patterson, Keith.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Engineering Aerospace.;Engineering General.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 126 p.
  • 总页数 126
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:53:52

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