{"created":"2023-06-20T15:19:09.596765+00:00","id":49535,"links":{},"metadata":{"_buckets":{"deposit":"2f3ae4a3-b6b1-41dc-a145-d0e4894324f0"},"_deposit":{"created_by":1,"id":"49535","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"49535"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00049535","sets":["1543:1693:2270","1887:1891"]},"author_link":["557822","557823","557824","557821"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Prototype evaluation of electrothermal acceleration type PPT applying sheet-type Teflon propellant supply mechanism"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2023-01","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"令和4年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium FY2022","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"令和4年度宇宙輸送シンポジウム（2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)) , 相模原市, 神奈川県","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Sheet propellant supply was applied to a pulsed plasma thruster (PPT) to maintain the impulse bits, which are usually lowered through tens of thousands of firings, and to prevent charring on the propellant surface, which causes operation failure. A ceramic cavity with grooves on the sides was designed to maintain the internal shape of the cavity even after thousands of pulsed arc discharge. Sheet propellants are supplied along the cavity sides so that the propellant surface is exposed to the plasma through the grooves. The prototype thruster generated 1000-shot firing.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA6000184079","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"STEP-2022-027","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所(JAXA)(ISAS)"}]},"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":"東京都立大学大学院"},{"subitem_text_value":"東京都立大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"}]},"item_5_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_ab4af688f83e57aa","subitem_version_type":"AM"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"溝井, 翔太"}],"nameIdentifiers":[{"nameIdentifier":"557821","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"各務, 聡"}],"nameIdentifiers":[{"nameIdentifier":"557822","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"MIZOI, Shota","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"557823","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"KAKAMI, Akira","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"557824","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2023-05-23"}],"displaytype":"detail","filename":"SA6000184079.pdf","filesize":[{"value":"563.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA6000184079.pdf","url":"https://jaxa.repo.nii.ac.jp/record/49535/files/SA6000184079.pdf"},"version_id":"575f70f5-00ce-4c55-9b2f-b50b913c4a85"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"シート状テフロン推進剤供給機構を適用した電熱加速型パルスプラズマスラスタの試作評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"シート状テフロン推進剤供給機構を適用した電熱加速型パルスプラズマスラスタの試作評価"}]},"item_type_id":"5","owner":"1","path":["1891","2270"],"pubdate":{"attribute_name":"公開日","attribute_value":"2023-05-23"},"publish_date":"2023-05-23","publish_status":"0","recid":"49535","relation_version_is_last":true,"title":["シート状テフロン推進剤供給機構を適用した電熱加速型パルスプラズマスラスタの試作評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T18:31:04.145836+00:00"}