{"created":"2023-06-20T14:39:18.736528+00:00","id":6048,"links":{},"metadata":{"_buckets":{"deposit":"f379d23a-be5e-4281-80e8-ad55af3c858c"},"_deposit":{"created_by":1,"id":"6048","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6048"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006048","sets":["1887:1893","9:789:998:1028"]},"author_link":["30132","30131"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study of water energy cycle space propulsion system"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-11-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"302","bibliographicPageStart":"297","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":"Water-Energy-Cycle Space Propulsion System was defined as a space system supporting long-term and large-scale space activity. On the test stand which can change a posture, the principle model was assembled, the posture was changed in +/- 1 G, and the performance of a principle model was compared. As a result of experimenting in +/- 1 G, when it operated normally in any case and it did separation of gas and a liquid on the level of each subsystem, under terrestrial gravity environment, it came out enough and a certain thing was understood. The feel referred to as operating satisfactory also under the micro-gravity environment of space was acquired as a result of consideration. The Proton Exchange Membrane (PEM) electrolyzer and the fuel cell which were used for the experiment made the regenerative fuel cell as an experiment, and used the single cell for this research in normal temperature. The phenomenon of ignition delay has been improved by the device of injection structure, and adjustment of injection timing in the catalyst ignition experiment of hydrogen/oxygen thruster. Moreover, it turns out that water adheres to the catalyst layer surface after a combustion end.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049500064","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　技術開発部"}]},"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 Space Technology Development Dept., Institute of Space and Astronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"橋本, 保成"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Yasunari","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":"49500064.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49500064.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6048/files/49500064.pdf"},"version_id":"0ca84ab0-89f9-4ba3-a281-6891e59d97e7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"宇宙機推進","subitem_subject_scheme":"Other"},{"subitem_subject":"水エネルギーサイクル","subitem_subject_scheme":"Other"},{"subitem_subject":"微小重力","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙環境","subitem_subject_scheme":"Other"},{"subitem_subject":"生命維持システム","subitem_subject_scheme":"Other"},{"subitem_subject":"エネルギー貯蔵","subitem_subject_scheme":"Other"},{"subitem_subject":"発電機","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"水素-酸素燃料電池","subitem_subject_scheme":"Other"},{"subitem_subject":"電解","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"water energy cycle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microgravity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"life support system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"energy storage","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric generator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hydrogen oxygen fuel cell","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electrolysis","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":"水サイクル宇宙推進システムの研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"水サイクル宇宙推進システムの研究"}]},"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":"6048","relation_version_is_last":true,"title":["水サイクル宇宙推進システムの研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:03:16.050443+00:00"}