{"created":"2024-01-26T03:44:18.915159+00:00","id":2000215,"links":{},"metadata":{"_buckets":{"deposit":"87fd0a23-51a5-463d-8594-3c31e4eda955"},"_deposit":{"created_by":27,"id":"2000215","owner":"27","owners":[27],"pid":{"revision_id":0,"type":"depid","value":"2000215"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:02000215","sets":["1398:1421:1706074693147","1887:1893","9:10:1695275225494:1706074364524"]},"author_link":[],"item_1692929429513":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":" Ammonium Dinitramide (ADN)-based ionic liquid propellants are promising new liquid propellants with excellent propulsive performance, stability, and ground handling characteristics. There have been studies on the properties of ADN-based ionic liquids alone and on thruster element technologies such as ignition systems and injectors. Our research group is currently studying chemical thrusters using ADN-based ionic liquids as propellant and is conducting ground burning tests for future space demonstrations. This report summarizes the status of the ground combustion test and the development plan up to the space demonstration.","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 Space and Astronautical Sciences, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2024-01-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"7","bibliographicPageStart":"5","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:JAXA- 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Propulsion","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を適用した化学スラスタの開発","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を適用した化学スラスタの開発","subitem_title_language":"ja"},{"subitem_title":"Development of Chemical Thrusters applying High Energetic Ionic Liquid Propellants","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":"2000215","relation_version_is_last":true,"title":["高エネルギーイオン液体推進剤を適用した化学スラスタの開発"],"weko_creator_id":"27","weko_shared_id":-1},"updated":"2024-01-31T02:00:55.391823+00:00"}