@inproceedings{oai:jaxa.repo.nii.ac.jp:00038660,
 author = {水谷, 忠均 and 山脇, 敏彦 and 小松, 敬治 and 後藤, 健 and 竹内, 伸介 and 松原, 英雄 and 中川, 貴雄 and 高井, 茂希 and 岡林, 明伸 and 楢崎, 勝弘 and Mizutani, Tadahito and Yamawaki, Toshihiko and Komatsu, Keiji and Goto, Ken and Takeuchi, Shinsuke and Nakagawa, Takao and Matsuhara, Hideo and Takai, Shigeki and Okabayashi, Akinobu and Narasaki, Katsuhiro},
 book = {第58回宇宙科学技術連合講演会講演集, Proceedings of 58th Space Sciences and Technology Conference},
 month = {Nov},
 note = {第58回宇宙科学技術連合講演会（2014年11月12日-15日. 長崎ブリックホール), 長崎市, 長崎県, The infrared space telescope SPICA, Space Infrared Telescope for Cosmology and Astrophysics, which features a 3m-class and 6K cryogenically cooled space telescope, is a next-generation astronomical project of Japan Aerospace Ex-ploration Agency (JAXA). The telescope and scientific instruments are cooled by a combination of an active (mechanical) cooling system and a passive (insulation and radiation) cooling system in the payload module. In this paper, the structural overview is described especially for the passive cooling system in the payload module and the summary of some experi-mental studies is presented., 資料番号: AC1500019000, レポート番号: JSASS-2014-4142},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {赤外線天文衛星SPICAのミッション部冷却システムの構造設計},
 year = {2014}
}