{"created":"2023-06-20T14:39:18.389923+00:00","id":6040,"links":{},"metadata":{"_buckets":{"deposit":"d4aaba6a-9c7f-4739-bfe1-6d11015ef845"},"_deposit":{"created_by":1,"id":"6040","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6040"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006040","sets":["1887:1893","9:789:998:1028"]},"author_link":["30065","30066"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of the fuel cell for aerospace applications"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-11-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"260","bibliographicPageStart":"257","bibliographicVolumeNumber":"JAXA-SP-06-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書"},{"bibliographic_title":"JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Japan Aerospace Exploration Agency (JAXA) is now developing polymer electrolyte fuel cell (PEFC) systems that can be applied to the high altitude balloon, transfer vehicle, and space craft. We designed the fuel cell system for low pressure environment where the working gases were supplied by the counter-flow method and the temperature of the system was passively controlled by the heat generated from the fuel cell stack. We assembled the system and are testing its performance under the thermal vacuum conditions. Furthermore, we started the development of a fuel cell system which can be operated by the propellants for spacecraft. We tried to operate the fuel cell using Hydrazine and Nitrogen Tetra Oxide. Through our measurements, stable generation of electricity was observed using PEFC. We also tried to measure the performance of the PEFC using the propellants with additives in order to decrease the melting point of the propellants.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049500056","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-06-006","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"曽根, 理嗣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sone, Yoshitsugu","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-16"}],"displaytype":"detail","filename":"49500056.pdf","filesize":[{"value":"596.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49500056.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6040/files/49500056.pdf"},"version_id":"f064ec7e-50fe-4245-9339-9ea13dea738c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高分子電解質燃料電池","subitem_subject_scheme":"Other"},{"subitem_subject":"水素-酸素燃料電池","subitem_subject_scheme":"Other"},{"subitem_subject":"加湿","subitem_subject_scheme":"Other"},{"subitem_subject":"電流密度","subitem_subject_scheme":"Other"},{"subitem_subject":"熱真空条件","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"polymer electrolyte fuel cell","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hydrogen oxygen fuel cell","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"humidification","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"current density","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal vacuum condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"航空宇宙用燃料電池に係る研究の新しい展開","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空宇宙用燃料電池に係る研究の新しい展開"}]},"item_type_id":"3","owner":"1","path":["1028","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6040","relation_version_is_last":true,"title":["航空宇宙用燃料電池に係る研究の新しい展開"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:03:27.389308+00:00"}