Kihm Hagyong, Yang Ho-Soon, Moon Il Kweon, Yeon Jeong-Heum, Lee Seung-Hoon, Lee Yun-Woo
Center for Space Optics, Korea Research Institute of Standards and Science, Daejeon, South Korea.
Appl Opt. 2012 Nov 10;51(32):7776-83. doi: 10.1364/AO.51.007776.
A new mirror mounting technique applicable to the primary mirror in a space telescope is presented. This mounting technique replaces conventional bipod flexures with flexures having mechanical shims so that adjustments can be made to counter the effects of gravitational distortion of the mirror surface while being tested in the horizontal position. Astigmatic aberration due to the gravitational changes is effectively reduced by adjusting the shim thickness, and the relation between the astigmatism and the shim thickness is investigated. We tested the mirror interferometrically at the center of curvature using a null lens. Then we repeated the test after rotating the mirror about its optical axis by 180° in the horizontal setup, and searched for the minimum system error. With the proposed flexure mount, the gravitational stress at the adhesive coupling between the mirror and the mount is reduced by half that of a conventional bipod flexure for better mechanical safety under launch loads. Analytical results using finite element methods are compared with experimental results from the optical interferometer. Vibration tests verified the mechanical safety and optical stability, and qualified their use in space applications.
提出了一种适用于空间望远镜主镜的新型镜面安装技术。这种安装技术用带有机械垫片的挠曲结构取代了传统的双足挠曲结构,以便在水平位置进行测试时能够进行调整,以抵消镜面重力畸变的影响。通过调整垫片厚度,有效地降低了重力变化引起的像散像差,并研究了像散与垫片厚度之间的关系。我们使用零透镜在曲率中心对镜面进行了干涉测量测试。然后,在水平设置中,将镜面绕其光轴旋转180°后重复该测试,并寻找最小系统误差。采用所提出的挠曲安装结构,镜体与安装结构之间粘合剂耦合处的重力应力比传统双足挠曲结构降低了一半,从而在发射载荷下具有更好的机械安全性。将有限元方法的分析结果与光学干涉仪的实验结果进行了比较。振动测试验证了其机械安全性和光学稳定性,并证明其适用于空间应用。