Design, fabrication and space suitability tests of wide field of view, ultra-compact, and high resolution telescope for space application

被引:11
|
作者
Tumarina, M. [1 ]
Ryazanskiy, M. [2 ]
Jeong, S. [1 ,3 ]
Hong, G. [1 ]
Vedenkin, N. [2 ,3 ]
Park, I. H. [1 ,3 ]
Milov, A. [2 ]
机构
[1] Sungkyunkwan Univ, Dept Phys, 27-501 2066 Seobu Ro, Suwon 16419, Gyeonggi Do, South Korea
[2] SatByul Co Ltd, 27-505 2066 Seobu Ro, Suwon 16419, Gyeonggi Do, South Korea
[3] Sungkyunkwan Univ, Inst Sci & Technol Space, 2066 Seobu Ro, Suwon 16419, Gyeonggi Do, South Korea
来源
OPTICS EXPRESS | 2018年 / 26卷 / 03期
基金
新加坡国家研究基金会;
关键词
D O I
10.1364/OE.26.002390
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
We report on the design, manufacture, and testing of an ultra-compact telescope for 16 unit (16U) CubeSats for Earth and space observation. This telescope provides 1 arcsec resolution at a 2.9 degree field of view. Dimensions are optimized to 230 x 230 x 330mm(3) with a mass of less than 6kg including support structure. Our catadioptric 5-element design consists of a full-aperture corrector, a Mangin primary mirror (PM), a secondary mirror (SM), and a 2-lens field corrector. The focal length is 745mm, and squared-circular aperture has an equivalent diameter of 241mm. The designed modulation transfer function (MTF) is 0.275 for the entire unit including baffles at a Nyquist frequency of 161 cycles/mm for the 450-800nm band. As one of the distinguishing features of our state-of-the-art design, all optical surfaces are spherical to simplify adjustment. For the best thermal stability, all optical elements are produced from fused silica. We describe the details of design, adjustment, and laboratory performance tests for space environments in accordance with the requirements for in-orbit operation onboard Earth-observation micro-satellites to be launched in 2018. (C) 2018 Optical Society of America under the terms of the OSA Open Access Publishing Agreement
引用
收藏
页码:2390 / 2399
页数:10
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