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空间大口径望远镜可展开镜片系统的概念设计
引用本文:王翔,张广宇,初昶波,胡玉禧,马德盛.空间大口径望远镜可展开镜片系统的概念设计[J].机械设计与研究,2004,20(6):49-52.
作者姓名:王翔  张广宇  初昶波  胡玉禧  马德盛
作者单位:中国科学技术大学,精密机械与精密仪器系,合肥,260026
基金项目:中科院创新基金资助项目,中国科学技术大学 985预研基金资助项目
摘    要:简要介绍下一代空间望远镜的可展开镜片系统的概念设计及其进展,以直径为2米的卡塞格林型望远镜为目标,对其主反射镜和次镜的可折叠、展开原理机构进行了初步分析,给出了利用点扩散函数来进行主镜剖分方式及其子镜形状选择的方法,从经典机构的角度,分别对主镜剖分后的子镜和次镜的展开、定位和锁紧等运动及其结构进行了分析和选择,给出了一种可展开空间望远镜的概念设计方案;最后,提出了需要进一步研究的关键问题。

关 键 词:概念设计  可展开结构  空间望远镜  空间光学
文章编号:1006-2343(2004)06-049-04
修稿时间:2004年6月21日

Concept Design for Deployable Large-aperture optical Structure of Space Telescopes
WANG Xiang,ZHANG Guang-yu,CHU Chang-bo,Hu Yu-xi,MA De-sheng.Concept Design for Deployable Large-aperture optical Structure of Space Telescopes[J].Machine Design and Research,2004,20(6):49-52.
Authors:WANG Xiang  ZHANG Guang-yu  CHU Chang-bo  Hu Yu-xi  MA De-sheng
Abstract:Large-aperture Space Telescopes is the development trend of the space optics in the future. This paper discussed the concept design and the researching progress for the deployable mirror system of the next generation space telescope. Regarding the Cassegrain telescope with 2m in diameter as the object, the mechanism of deployable primary mirror and secondary mirror original structure was analyzd. The method of the division of primary mirror and the selected shape of segments was demonstrated by point spread function. From the point of view of classical mechanism, the analysis of the segmented primary mirror and secondary mirror, deployment, positioning-lock mechanism and its structure was made individually. A new concept design for deployable space telescope was presented. Finally, the authors propose the key problems which need further research.
Keywords:concept design  deployable structure  space telecopes  space optics
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