{"created":"2023-06-20T14:43:59.461451+00:00","id":11374,"links":{},"metadata":{"_buckets":{"deposit":"8de738ae-bee2-44b1-9688-b8939a5a0767"},"_deposit":{"created_by":1,"id":"11374","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"11374"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00011374","sets":["1543:1580:1594","1887:1891"]},"author_link":["99956","99963","99961","99957","99962","99954","99960","99958","99959","99955"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Next generation thermal control technology for spacecraft using advanced materials"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"504","bibliographicPageStart":"503","bibliographic_titles":[{"bibliographic_title":"第5回宇宙科学シンポジウム"},{"bibliographic_title":"Proceedings of the 5th Space Science Symposium","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"宇宙機ミッションの多様化に伴い熱制御技術の高度化・高効率化が望まれている。宇宙機熱制御技術の向上を図るため、著者らはこれまで先進材料を用いた放射率可変素子(SRD)や自律型吸放熱デバイス(RTP)の開発を行ってきた。本稿では、2004年度より研究を開始した多孔質ポリイミドや熱電酸化物などの先進材料を用いた次世代熱制御技術の開発について、アプリケーションの提案および熱物性計測手法について報告する。","subitem_description_type":"Abstract"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049122120","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"慶應義塾大学 大学院理工学研究科"},{"subitem_text_value":"東海大学"},{"subitem_text_value":"東海大学"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Keio University Graduate School of Science & Technology"},{"subitem_text_language":"en","subitem_text_value":"Tokai University"},{"subitem_text_language":"en","subitem_text_value":"Tokai University"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only 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conductivity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electrical resistivity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Seebeck coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal insulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal resistance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermoelectric generator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermoelectric pumped loop","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"periodic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"self cooling 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