2009
DOI: 10.5303/pkas.2009.24.1.053
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Development of the Mechanical Structure of the Miris Soc

Abstract: MIRIS is the main payload of the STSAT-3 (Science and Technology Satellite 3) and the first infrared space telescope for astronomical observation in Korea. MIRIS space observation camera (SOC) covers the observation wavelength from 0.9㎛ to 2.0㎛ with a wide field of view 3.67˚☓3.67˚. The PICNIC HgCdTe detector in a cold box is cooled down below 100K by a micro Stirling cooler of which cooling capacity is 220mW at 77K. MIRIS SOC adopts passive cooling technique to chill the telescope below 200 K by pointing to t… Show more

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“…Fig. 1 shows the SOC and the main goal of the SOC is near infrared imaging surveying in the equatorial areas of our galaxy and Cosmic Infrared Background (CIB) observation in North Ecliptic Pole (NEP) and South Ecliptic Pole (SEP) in the 0.9 ~ 2.0 um wavelength range [7,8]. The Winston cone baffle is the baffle design for the SOC.…”
Section: Introductionmentioning
confidence: 99%
“…Fig. 1 shows the SOC and the main goal of the SOC is near infrared imaging surveying in the equatorial areas of our galaxy and Cosmic Infrared Background (CIB) observation in North Ecliptic Pole (NEP) and South Ecliptic Pole (SEP) in the 0.9 ~ 2.0 um wavelength range [7,8]. The Winston cone baffle is the baffle design for the SOC.…”
Section: Introductionmentioning
confidence: 99%