4.1 Article

The Infrared Camera (IRC) for AKARI -: Design and imaging performance

Journal

PUBLICATIONS OF THE ASTRONOMICAL SOCIETY OF JAPAN
Volume 59, Issue -, Pages S401-S410

Publisher

OXFORD UNIV PRESS
DOI: 10.1093/pasj/59.sp2.S401

Keywords

infrared : general; instrumentation : detectors; space vehicles : instruments

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The Infrared Camera (IRC) is one of two focal-plane instruments on the AKARI satellite. It is designed for wide-field deep imaging and low-resolution spectroscopy in the near- to mid-infrared (1.8-26.5 mu m) in the pointed observation mode of AKARI. The IRC is also operated in the survey mode to make an All-Sky Survey at 9 and 18 Am. It comprises three channels. The NIR channel (1.8-5.5 mu m) employs a 512 x 412 InSb array, whereas both the MIR-S (4.6-13.4 mu m) and MIR-L (12.6-26.5 mu m) channels use 256 x 256 Si:As impurity band conduction arrays. Each of the three channels has a field-of-view of about 10' x 10' and they are operated simultaneously. The NIR and MIR-S share the same field-of-view by virtue of a beam splitter. The MIR-L observes the sky about 25' away from the NIR/MIR-S field-of-view. The IRC gives us deep insights into the formation and evolution of galaxies, the evolution of planetary disks, the process of star-formation, the properties of interstellar matter under various physical conditions, and the nature and evolution of solar system objects. The in-flight performance of the IRC has been confirmed to be in agreement with the pre-flight expectation. This paper summarizes the design and the in-flight operation and imaging performance of the IRC.

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