{"created":"2023-06-20T14:48:28.922580+00:00","id":16292,"links":{},"metadata":{"_buckets":{"deposit":"e06a2bba-2967-400e-abbb-622e8c81fecc"},"_deposit":{"created_by":1,"id":"16292","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16292"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016292","sets":["1543:1693:1700","1887:1891"]},"author_link":["147800","147796","147801","147806","147798","147805","147803","147797","147807","147802","147799","147804"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Performance Prediction of Electrothermal Pulsed Plasma Thrusters for the 1st and 2nd Osaka Institute of Technology PROITERES Satellites by Numerical Calculation"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-01","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"平成24年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium: FY2012","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":"平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18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 FY2012 (January 17-18, 2013. 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":"The Project of Osaka-Institute-of-Technology Electric-Rocket-Engine onboard Small Space Ship (PROITERES) was started at Osaka Institute of Technology in 2007. In PROITERES, a 14.5-kg nano satellite with electrothermal pulsed plasma thrusters (PPT) was launched on September 9th 2012. The main mission is powered flight of nano satellite by electric thruster itself. Now, we will be trying to establish a contact to satellite. After establishing satellite ignitions by command the thruster will be operated from the ground. In this paper, the performance is predicted by numerical simulation and ground experiment. Furthermore, the 2nd PROITERES satellite with high-power PPT systems was introduced.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"},{"subitem_description":"形態: PDF","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"},{"subitem_description":"Physical characteristics: PDF","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0061856156","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: STEP-2012-073","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":"大阪工業大学"},{"subitem_text_value":"大阪工業大学"},{"subitem_text_value":"大阪工業大学"},{"subitem_text_value":"大阪工業大学"},{"subitem_text_value":"大阪工業大学"},{"subitem_text_value":"ハイサーブ"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Osaka Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Osaka Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Osaka Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Osaka Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"-"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"陳, 煥俊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村岡, 力夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 慎人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"木咲, 秀彌"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田原, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"脇園, 堯"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Chen, Huanjun","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Muraoka, Rikio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Masato","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kisaki, Shuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tahara, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakizono, Takashi","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":"2020-01-20"}],"displaytype":"detail","filename":"61856156.pdf","filesize":[{"value":"546.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61856156.pdf","url":"https://jaxa.repo.nii.ac.jp/record/16292/files/61856156.pdf"},"version_id":"5b933e2e-5e8c-4221-b440-8e0c32ccaae2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Electric Propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Pulsed Plasma Thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Nano Satellite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Powered Flight","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"数値計算による大阪工業大学プロイテレス衛星1、2号機搭載電熱加速型パルスプラズマスラスタの性能予測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"数値計算による大阪工業大学プロイテレス衛星1、2号機搭載電熱加速型パルスプラズマスラスタの性能予測"}]},"item_type_id":"5","owner":"1","path":["1700","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16292","relation_version_is_last":true,"title":["数値計算による大阪工業大学プロイテレス衛星1、2号機搭載電熱加速型パルスプラズマスラスタの性能予測"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:55:20.047260+00:00"}