{"created":"2023-06-20T14:35:46.277827+00:00","id":2045,"links":{},"metadata":{"_buckets":{"deposit":"e1f87af9-9369-49f4-bcfb-8df715684529"},"_deposit":{"created_by":1,"id":"2045","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2045"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002045","sets":["1398:1421:1429","1887:1893","9:10:97:101"]},"author_link":["2560","2565","2563","2570","2568","2559","2566","2569","2567","2562","2564","2561"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"7","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-11-005","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: 平成23年度研究成果研究成果報告書"},{"bibliographic_title":"JAXA Research and Development Report: Collaborative Research Activity on Energetic Materials Research Report FY2011","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Ammonium perchrolate (AP) is the most useful oxidizer for the solid rocket motors (SRMs) under the present situation, however it is also the source of the environmental pollution close to the launch site. It is well known that HCI is exhausted through the firing of SRMs and its concentration reaches approximately 10 to 20 mole percent of the total exhaust. \"Environmentaly friendly\" and \"High performance\" are required for the next-generation SRMs. In this study, ammonium dinitramide (ADN), which has recently attracted attentions as a halogen-free oxidizer was employed for a substitution of AP and the combustion properties of the composite propellants were investigated. Thermoplastic elastomer (TP) and hydroxyl-terminated butadiene polymer (HTPB) were used as a binder for this research. Pyrotechnic sensitivity analysis was conducted to estimate the safety of TP/ADN propellants. Strand burning tests were also carried out for all samples and the burning rate and temperature profile were obtained through these experiments. It was found that the burning rate characteristics of ADN-based propellants were influenced by the binders.","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: AA0065204001","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-11-005","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"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":"東京大学大学院"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)"},{"subitem_text_value":"細谷火工"},{"subitem_text_value":"細谷火工"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Graduate School, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Hosoya Pyro-Engineering"},{"subitem_text_language":"en","subitem_text_value":"Hosoya Pyro-Engineering"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"藤里, 公司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"羽生, 宏人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"芝本, 秀文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"于, 秀超"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三宅, 淳巳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"堀, 恵一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujisato, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Habu, Hiroto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shibamoto, Hidefumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yu, Xiuchao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyake, Atsumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hori, Keiichi","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":"2020-01-15"}],"displaytype":"detail","filename":"65204001.pdf","filesize":[{"value":"903.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65204001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2045/files/65204001.pdf"},"version_id":"855c0623-2997-4e57-b3cd-bb1ced3ce278"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Combustion characteristics of ADN-based solid propellants","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Combustion characteristics of ADN-based solid propellants","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["101","1429","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2045","relation_version_is_last":true,"title":["Combustion characteristics of ADN-based solid propellants"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:29:41.143417+00:00"}