{"created":"2023-06-20T15:18:04.127939+00:00","id":48285,"links":{},"metadata":{"_buckets":{"deposit":"128bbf7e-16ca-469c-8b16-3d754e2bd7ab"},"_deposit":{"created_by":1,"id":"48285","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"48285"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00048285","sets":["1398:1421:2192","1887:1893","9:10:2138:2170"]},"author_link":["544792","544791","544793","544795","544794","544796"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A Concept of the Small Chemical Thruster with High Energetic Ionic Liquids"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2022-02-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"8","bibliographicPageStart":"6","bibliographicVolumeNumber":"JAXA-RR-21-002","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: 令和3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 (2021)","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"アンモニウムジニトラミドを基材とするイオン液体系推進剤 (ADN-EILPs) は，低毒・高密度比推力が期待される有望な一液推進剤の一つである．これまで筆者らは，ADN-EILPs が内包する点火・着火特性に関連する技術課題の克服に取り組んできた．昨今の研究により，新たな点火方式として，レーザ輻射加熱機構とレーザ吸光材の組み合わせを考案し， ADN-EILPs の効果的な点火の糸口を見出すまでに至った．本報告では，これら点火に関連する研究の展開として，当該点火機構に新たな推進剤供給機構を組み合わせた，ADN-EILPs を用いるスラスタの概念について紹介する．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Ammonium dinitramide-based ionic liquid propellants (ADN-EILPs) are expected the candidates with high-performance and low toxicity for next-generation chemical thruster in small satellites. Authors have investigated the ignition of ADN-EILPs to solve technical problems for thruster applications, e.g. ignitor or ignition mechanism of ADN-EILPs. Through the past studies, the combination of laser radiant heating and carbon-based laser absorbent was found out as a solution of expected ignition methods for ADN-EILPs. This paper introduces a thruster concept using ADN-EILPs by utilizing the new propellant supply method as well as such the ignition mechanism.","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: AA2130019002","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-21-002","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/00048269","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":"名古屋大学"},{"subitem_text_value":"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":"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)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_3_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"伊東山, 登"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"和田, 明哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"羽生, 宏人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ITOUYAMA, Noboru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"WADA, Asato","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HABU, Hiroto","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":"2022-02-04"}],"displaytype":"detail","filename":"AA2130019002.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA2130019002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/48285/files/AA2130019002.pdf"},"version_id":"0bc3b55c-7e7d-45ca-b94a-a3d8b97d8fd2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Ammonium dinitramide","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Ionic liquid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Laser ignition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Small thruster system","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":"高エネルギイオン液体推進剤の小型スラスタ概念設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高エネルギイオン液体推進剤の小型スラスタ概念設計"}]},"item_type_id":"3","owner":"1","path":["1893","2170","2192"],"pubdate":{"attribute_name":"公開日","attribute_value":"2022-02-04"},"publish_date":"2022-02-04","publish_status":"0","recid":"48285","relation_version_is_last":true,"title":["高エネルギイオン液体推進剤の小型スラスタ概念設計"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:22:24.508251+00:00"}