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        <title>Thermal Imaging Performance of TIR Onboard the Hayabusa2 Spacecraft</title>
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            <author_list>Arai, Takehiko; Nakamura, Tomoki; Tanaka, Satoshi; Demura, Hirohide; Ogawa, Yoshiko; Sakatani, Naoya; Horikawa, Yamato; Senshu, Hiroki; Fukuhara, Tetsuya; Okada, Tatsuaki</author_list>
            <publication_year>2017</publication_year>
            <doi>10.1007/s11214-017-0353-9</doi>
            <keyword>Hayabusa2</keyword>
            <keyword>TIR</keyword>
            <keyword>Infrared camera</keyword>
            <keyword>Thermography</keyword>
            <keyword>Thermal emissivity</keyword>
            <keyword>Surface roughness</keyword>
            <keyword>Thermal inertia</keyword>
            <keyword>Ryugu</keyword>
            <keyword>1999 JU3</keyword>
            <keyword>Asteroid</keyword>
            <keyword>Carbonaceous chondrite</keyword>
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                This document is a final accepted version of the paper before publication.
                The published version is available at https://doi.org/10.1007/s11214-017-0353-9 .
                Published version: Space Science Reviews, Volume 208, Issue 1-4, pp. 239-254, 2017.
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        <copyright>The Author(s) 2017</copyright>
        <publication_date>2017-03-28</publication_date>
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