空间任务中大型膜式遮阳板展开与折叠技术研究现状

Lin Qiuhong, Peng Tao, Su Zhou, Qiu Hui, Li Xiao, Cong Qiang
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引用次数: 0

摘要

高分辨率观测需要设计孔径越来越大的太空望远镜。基本上需要更大但不是更重的可展开遮阳板。由于薄膜结构具有储存体积小、重量轻等优点,可以满足大型薄膜遮阳板设计的苛刻要求,逐渐成为当前的研究热点。本文从机械驱动展开、弹性展开和充气展开三个方面综述了遮阳板展开技术的研究进展。比较了不同几何形状薄膜遮阳板的折叠方法,总结了薄膜折叠技术的研究现状。该综述对未来遮阳板的部署和折叠技术提出了一些建议。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

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Research Status of Deployment and Folding Technology of Large-Scale Membrane Sunshield in Space Mission

High-resolution observation requires the design of space telescopes with larger and larger aperture. Larger but not heavier deployable sunshields are essentially needed. Due to the advantages such as smaller storage volume and lightweight, the membrane structure can meet the demanding requirements of the design of larger membrane sunshields and has gradually become a current research hotspot. This paper summarizes the research progresses of sunshield deployment technology from three categories: mechanically driven deployment, elastic deployment, and inflatable deployment. The folding methods of membrane sunshields with different geometric shapes are compared, and the research status of membrane folding technology is summarized. The summary gives some suggestions on future sunshield deployment and folding technology.

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