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Cited 6 time in webofscience Cited 9 time in scopus
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Design, fabrication and space suitability tests of wide field of view, ultra-compact, and high resolution telescope for space applicationopen access

Authors
Tumarina, M.[Tumarina, M.]Ryazanskiy, M.[Ryazanskiy, M.]Jeong, S.[Jeong, S.]Hong, G.[Hong, G.]Vedenkin, N.[Vedenkin, N.]Park, I.H.[Park, I.H.]Milov, A.[Milov, A.]
Issue Date
5-Feb-2018
Publisher
OSA - The Optical Society
Citation
Optics Express, v.26, no.3, pp.2390 - 2399
Indexed
SCIE
SCOPUS
Journal Title
Optics Express
Volume
26
Number
3
Start Page
2390
End Page
2399
URI
https://scholarworks.bwise.kr/skku/handle/2021.sw.skku/25693
DOI
10.1364/OE.26.002390
ISSN
1094-4087
Abstract
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 × 230 × 330mm3 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. © 2018 Optical Society of America
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