Bulletin of the Korean Space Science Society (한국우주과학회:학술대회논문집(한국우주과학회보))
- 2008.10a
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- Pages.27.1-27.1
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- 2008
Discussion of Preliminary Design Review for MIRIS, the Main Payload of STSAT-3
- Han, Won-Yong (Korea Astronomy and Space Science Institute) ;
- Jin, Ho (Korea Astronomy and Space Science Institute) ;
- Park, Jang-Hyun (Korea Astronomy and Space Science Institute) ;
- Nam, Uk-Won (Korea Astronomy and Space Science Institute) ;
- Yuk, In-Soo (Korea Astronomy and Space Science Institute) ;
- Lee, Sung-Ho (Korea Astronomy and Space Science Institute) ;
- Park, Young-Sik (Korea Astronomy and Space Science Institute) ;
- Park, Sung-Jun (Korea Astronomy and Space Science Institute) ;
- Lee, Dae-Hee (Korea Astronomy and Space Science Institute) ;
- Ree, Chang-H. (Korea Astronomy and Space Science Institute) ;
- Jeong, Woong-Seob (Korea Astronomy and Space Science Institute) ;
- Moon, Bong-Kon (Korea Astronomy and Space Science Institute) ;
- Cha, Sang-Mok (Korea Astronomy and Space Science Institute) ;
- Cho, Seoung-Hyun (Korea Astronomy and Space Science Institute) ;
- Rhee, Seung-Woo (Korea Aerospace Research Institute) ;
- Park, Jong-Oh (Korea Aerospace Research Institute) ;
- Lee, Seung-Heon (Korea Aerospace Research Institute) ;
- Lee, Hyung-Mok (Seoul National University) ;
- Matsumoto, Toshio (Seoul National University)
- Published : 2008.10.22
Abstract
KASI (Korea Astronomy and Space Science Institute) is developing a compact wide-field survey space telescope system, MIRIS (The Multi-purpose IR Imaging System) to be launched in 2010 as the main payload of the Korea Science and Technology Satellite 3. Through recent System Design Review (SDR) and Preliminary Design Review (PDR), most of the system design concept was reviewed and confirmed. The near IR imaging system adopted short F/2 optics for wide field low resolution observation at wavelength band 0.9~2.0 um minimizing the effect of attitude control system. The mechanical system is composed of a cover, baffle, optics, and detector system using a
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