{"created":"2023-06-20T14:35:36.969862+00:00","id":1867,"links":{},"metadata":{"_buckets":{"deposit":"b1cc53b6-8aed-4ee0-8731-85a797ffc6e0"},"_deposit":{"created_by":1,"id":"1867","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1867"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001867","sets":["1398:1421:1424","1887:1893","9:10:39:48"]},"author_link":["476516","476510","476515","476511","476506","476513","476509","476508","476517","476514","476507","476512"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Prediction of ignition delay of ADN-based ionic liquid propellants using thermal analysis"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-03-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"36","bibliographicPageStart":"31","bibliographicVolumeNumber":"JAXA-RR-16-006","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28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 (2016)","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系イオン液体(ADN系EILPsH)は比推力の高さ, 融点, 毒性の低さから次世代のスラスタ用一液式推進剤として実用化に向けた研究が進められている。本研究の目的は燃焼制御技術確立に向けADN系EILPsの加熱速度に対する着火遅れ時間と燃焼温度予測手法を構築することである。着火遅れ時間および燃焼温度予測手法は各種熱分析手法と燃焼シミュレーションとの組み合わせより構築した。本研究の予測結果から, 着火遅れ時聞は50-600Ks(exp -1)で加熱した場合0.5-4.5s 燃焼温度は約2000度Cとなった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Ammonium dinitramide based ionic liquid propellants have been studied as monopropellant in terms of high specific impulse, low melting point and low toxicity. The purpose of this study is construction prediction method of ignition delay and combustion temperature against heating rate of propellants for establishment of combustion control technique. The prediction method of ignition delay and combustion temperature is constructed by combination of thermal analysis method and combustion simulation. From the result of prediction, ignition delay is 0.5-4.5 s and combustion temperature is around 2000 C in the case of heating rate is 50-600 Ks(exp -1).","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: AA1630043005","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-16-006","subitem_description_type":"Other"}]},"item_3_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.20637/JAXA-RR-16-006/0005","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_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"福岡大学"},{"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":"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":"Yokohama National University"},{"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":"Fukuoka 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":"Yokohama National University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"早田, 葵"}],"nameIdentifiers":[{"nameIdentifier":"476506","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"塩田, 謙人"}],"nameIdentifiers":[{"nameIdentifier":"476507","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"伊里, 友一朗"}],"nameIdentifiers":[{"nameIdentifier":"476508","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"松永, 浩貴"}],"nameIdentifiers":[{"nameIdentifier":"476509","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"羽生, 宏人"}],"nameIdentifiers":[{"nameIdentifier":"476510","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"三宅, 淳巳"}],"nameIdentifiers":[{"nameIdentifier":"476511","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hayata, Mamoru","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476512","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Shiota, Kento","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476513","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Izato, Yuichiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476514","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Matsunaga, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476515","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Habu, Hiroto","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476516","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Miyake, Atsumi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"476517","nameIdentifierScheme":"WEKO"}]}]},"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":"AA1630043005.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630043005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1867/files/AA1630043005.pdf"},"version_id":"7ccb5a0d-063b-439e-99c8-338be9bb875f"}]},"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":"Energetic ionic liquid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Ignition delay","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Kinetics analysis","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":"熱特性解析によるアンモニウムジニトラミド系イオン液体の着火遅れ時間予測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"熱特性解析によるアンモニウムジニトラミド系イオン液体の着火遅れ時間予測"}]},"item_type_id":"3","owner":"1","path":["48","1424","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-03-23"},"publish_date":"2017-03-23","publish_status":"0","recid":"1867","relation_version_is_last":true,"title":["熱特性解析によるアンモニウムジニトラミド系イオン液体の着火遅れ時間予測"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:37:48.002597+00:00"}