期刊文献+

空间可展开主镜技术途径研究 被引量:3

Technical Ways for the Space Deployable Primary Mirror
下载PDF
导出
摘要 可展开光学系统是实现特大口径光学遥感器的技术途径之一。可展开光学系统的主要特点是主镜分块、收拢发射、入轨展开,并且主镜超轻量化。文章主要介绍了实现可展开光学系统主镜的两种方法(超轻分块镜和超轻超薄分块镜),并对两者的实现难易程度进行了比较。 The deployable optics was an effective way to realize the large aperture optics. The main characteristic of the deployable optic was the primary mirror. The primary mirror was segmented, folded when launch and deployed in orbit. This paper gave two ways to realize the segmented primary mirror, one was the ultra-light semi - rigid mirror and the other was the ultra-light and ultra- thin active mirror.
出处 《航天返回与遥感》 2008年第1期23-27,共5页 Spacecraft Recovery & Remote Sensing
关键词 可展开主镜 半刚性镜 超轻超薄主动镜 空间相机 Deployable primary mirror Ultra - light semi - rigid mirror Ultra - light and ultra - thin activemirror Space camera
  • 相关文献

参考文献3

二级参考文献3

  • 1R, G. Lyon, J. E, Dorband and J, M. Hollis. Computational complexity in space based optical syatems. SPIE 4056(2000).
  • 2Max E. Nein, Jon F. Lawrence. Monolithic vs. Deployable Primary Mirror Trade Considerations for the Next Generation Space Telescope. May 8, 2002.
  • 3王金堂,乌崇德.国外几种星载光学遥感器的发展情况简介[J].航天返回与遥感,2002,23(2):15-20. 被引量:9

共引文献27

同被引文献23

引证文献3

二级引证文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部