{"created":"2023-06-20T14:35:33.494314+00:00","id":1784,"links":{},"metadata":{"_buckets":{"deposit":"3a36b363-6f69-4e18-935d-74c1f0083a62"},"_deposit":{"created_by":1,"id":"1784","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1784"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001784","sets":["1398:1421:1422","1887:1893","9:10:13:19"]},"author_link":["475721","475732","475728","475725","475723","475727","475722","475731","475733","475720","475726","475724","475734","475729","475719","475730"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Research and development of thruster with high energetic ionic liquid and laser ignition"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2019-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"9","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-18-006","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 平成30年度研究成果報告書"},{"bibliographic_title":"JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2018)","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"エネルギー物質を基剤としたイオン液体はヒドラジンに代わる新しい液体推進剤として期待される．我々は高エネルギー物質アンモニウムジニトラミド（ADN）を基剤としたイオン液体推進剤（EILPs）を用いた新規スラスタシステムを実現するために，物性，スラスタ内での燃焼挙動，点火方式について研究を進めている．物性研究では，低融点かつ高性能であるEILPsの調製方法を明らかにした．既存方式を用いたスラスタ燃焼試験では微粒化および安定した燃焼を達成でき，EILPsのスラスタ用推進剤としての実現可能性が示された．また，新規点火方式について検討し，EILPsのレーザー点火を可能にした．以上の結果から，新しい概念のスラスタが見出された．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Ionic liquid based on high energetic materials is promising new liquid propellant replacing hydrazine. We have been studying physical properties, combustion behavior in thruster chamber, and ignition method for ammonium dinitramide (ADN)-based energetic liquid propellants (EILPs) to realize new thruster system. Our studies for physical properties enabled to prepare ADN-based EILPs with low melting point and high specific impulse. ADN-based EILPs could be atomized and stably combusted in thruster chamber with existing methods. We are studying new ignition method and enable to ignite ADN-based EILPs by laser. These results indicated completely new type of thruster system.","subitem_description_type":"Other"}]},"item_3_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"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1830031001","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-RR-18-006","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/JAXA-RR-18-006/0001","subitem_identifier_reg_type":"JaLC"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2216","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"福岡大学"},{"subitem_text_value":"東京大学"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"長岡技術科学大学"},{"subitem_text_value":"横浜国立大学 : 宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS)"},{"subitem_text_value":"福岡大学"},{"subitem_text_value":"横浜国立大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fukuoka University"},{"subitem_text_language":"en","subitem_text_value":"The University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"},{"subitem_text_language":"en","subitem_text_value":"Nagaoka University of Technology"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University : Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Fukuoka University"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"松永, 浩貴"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊東山, 登"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塩田, 謙人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊里, 友一朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"勝身, 俊之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"羽生, 宏人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 賢"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三宅, 淳巳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsunaga, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Itouyama, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shiota, Kento","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Izato, Yuichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katsumi, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Habu, Hiroto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Masaru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyake, Atsumi","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":"2020-01-31"}],"displaytype":"detail","filename":"AA1830031001.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1830031001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1784/files/AA1830031001.pdf"},"version_id":"40b47690-dd83-4640-aa2d-b3429f504f30"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Energetic Ionic Liquid Propellants (EILPs)","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"High Energetic Materials","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Ammonium Dinitramide (ADN)","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Laser Ignition","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":"高エネルギーイオン液体推進剤およびレーザー点火を用いた次世代スラスタの研究開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高エネルギーイオン液体推進剤およびレーザー点火を用いた次世代スラスタの研究開発"}]},"item_type_id":"3","owner":"1","path":["19","1422","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-02-28"},"publish_date":"2019-02-28","publish_status":"0","recid":"1784","relation_version_is_last":true,"title":["高エネルギーイオン液体推進剤およびレーザー点火を用いた次世代スラスタの研究開発"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T20:22:19.069547+00:00"}