Bulletin of the Korean Space Science Society (한국우주과학회:학술대회논문집(한국우주과학회보))
- 2009.10a
- /
- Pages.44.3-44.3
- /
- 2009
Discussion of Critical Design Review (CDR) for MIRIS, the Main Payload of STSAT-3
- Han, Won-Yong (Korea Astronomy & Space Science Institute (KASI)) ;
-
Lee, Dae-Hee
(Korea Astronomy & Space Science Institute (KASI))
;
- Nam, Uk-Won (Korea Astronomy & Space Science Institute (KASI)) ;
- Park, Young-Sik (Korea Astronomy & Space Science Institute (KASI)) ;
- Jeong, Woong-Seob (Korea Astronomy & Space Science Institute (KASI)) ;
- Ree, Chang-Hee (Korea Astronomy & Space Science Institute (KASI)) ;
- Moon, Bong-Kon (Korea Astronomy & Space Science Institute (KASI)) ;
- Park, Sung-Joon (Korea Astronomy & Space Science Institute (KASI)) ;
- Cha, Sang-Mok (Korea Astronomy & Space Science Institute (KASI)) ;
- Park, Jang-Hyun (Korea Astronomy & Space Science Institute (KASI)) ;
- Lee, Duk-Hang (Korea Astronomy & Space Science Institute (KASI)) ;
- Ka, Nung-Hyun (Korea Astronomy & Space Science Institute (KASI)) ;
- Lee, Mi-Hyun (Korea Astronomy & Space Science Institute (KASI)) ;
- Seon, Kwang-Il (Korea Astronomy & Space Science Institute (KASI)) ;
- Yuk, In-Soo (Korea Astronomy & Space Science Institute (KASI)) ;
-
Yang, Sun-Choel
(Korea Basic Science Institute (KBSI))
;
- Park, Jog-Oh (Korea Aerospace Research Institute(KARI)) ;
- Rhee, Seung-Wuh (Korea Aerospace Research Institute(KARI)) ;
-
Lee, Hyung-Mok
(Seoul Natinal University (SNU))
;
- Matsumoto, Toshio (Seoul Natinal University (SNU))
- Published : 2009.10.15
Abstract
The MIRIS (Multi-purpose IR Imaging System), as the main payload of Science and Technology Satellite-3 (STSAT-3), is being developed by KASI in collaboration with several institutes for wide-field space observation in near IR wavelength. The Engineering Qualification Model (EQM) of MIRIS has been designed and fabricated in the laboratory. The system performance tests have been made including opto-mechanics, vibration test, thermal-vacuum environmental test and passive cooling test down to 200K. Most of the performance test results were satisfied with system requirements. The results of MIRIS performance tests have been presented at Critical Design Review (CDR) on September 2009. Several revisions were also recommended for Flight Model (FM) design, and detailed plan to develop FM of MIRIS is discussed in this paper.
Keywords