{"created":"2024-01-26T03:44:11.599685+00:00","id":2000214,"links":{},"metadata":{"_buckets":{"deposit":"2b45ef06-9169-4315-b5a9-c10add5dc3ec"},"_deposit":{"created_by":27,"id":"2000214","owner":"27","owners":[27],"pid":{"revision_id":0,"type":"depid","value":"2000214"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:02000214","sets":["1398:1421:1706074693147","1887:1893","9:10:1695275225494:1706074364524"]},"author_link":[],"item_1692929429513":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":" We are conducting research and development of chemical propulsion systems for satellites using ammonium dinitramide (ADN)-based energetic ionic liquids (EILs) as propellants. They are expected to be used as propellants for high-performance and safe nano-satellite propulsion systems. The project aims to demonstrate the EILs in orbit within a few years, and this year, in parallel with the development of new thruster systems using laser and electrolytic ignition, and the advancement of new EILs-specific technologies such as the design of highly reactive ADN-based EILs, a prototype thruster using a simple method was built and a ground combustion test was conducted. The thruster has been tested in ground combustion tests. In the future, we plan to demonstrate the thruster's propulsion performance to clarify its feasibility as a chemical propulsion system, and then proceed with the fabrication of a thruster equipped with each new technology.","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1692929640552":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_language":"ja","subitem_description_type":"Other"},{"subitem_description":"Physical  characteristics: Original contains color illustrations","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1693474141533":{"attribute_name":"資料番号(Local)","attribute_value_mlt":[{"subitem_relation_type_id":{"subitem_relation_type_id_text":"資料番号: 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Academy"},{"subitem_text_language":"en","subitem_text_value":"Institute of Materials and Systems for Sustainability, Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Nihon University"},{"subitem_text_language":"en","subitem_text_value":"Fukuoka University"},{"subitem_text_language":"en","subitem_text_value":"Faculty of Environment and Information Sciences, Yokohama Naational University"},{"subitem_text_language":"en","subitem_text_value":"Nagaoka University of Technology"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Sciences, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Fukuoka University"},{"subitem_text_language":"en","subitem_text_value":"Faculty of Environment and Information Sciences, Yokohama Naational University"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2024-01-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"4","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-23-005","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5年度研究成果報告書","bibliographic_titleLang":"ja"},{"bibliographic_title":"JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2023)","bibliographic_titleLang":"en"}]}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: 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University","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"三宅, 淳巳","creatorNameLang":"ja"},{"creatorName":"MIYAKE, Atsumi","creatorNameLang":"en"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2023-01-30"}],"filename":"AA2330014001.pdf","format":"application/pdf","mimetype":"application/pdf","url":{"url":"https://jaxa.repo.nii.ac.jp/record/2000214/files/AA2330014001.pdf"},"version_id":"0a580c77-c4b0-44e6-81b9-db12288de9af"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Monopropellant","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Thruster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Micro Propulsion System","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"High Energetic 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System","subitem_title_language":"en"}]},"item_type_id":"40003","owner":"27","path":["1893","1706074693147","1706074364524"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2024-01-30"},"publish_date":"2024-01-30","publish_status":"0","recid":"2000214","relation_version_is_last":true,"title":["超小型衛星を見据えた高エネルギーイオン液体推進系の研究開発"],"weko_creator_id":"27","weko_shared_id":-1},"updated":"2024-01-31T02:00:47.864868+00:00"}