{"created":"2023-06-20T14:48:40.390551+00:00","id":16493,"links":{},"metadata":{"_buckets":{"deposit":"275d2983-64a5-4302-8c5b-222e83f27899"},"_deposit":{"created_by":1,"id":"16493","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16493"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016493","sets":["1543:1693:1702","1887:1891"]},"author_link":["149782","149781","149786","149783","149785","149780","149784","149787","149788","149789"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The Development of Low Melting Temperature Thermoplastic Propellant (LTP) with Aluminum Addition for the Next Generation Solid Rocket"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"平成22年度宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium: FY2010","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Authors have developed low melting temperature thermoplastic propellant (LTP) for the Next Generation Solid Rocket by using thermoplastic elastomer. For more improvement performance, aluminum (Al) addition to LTP was studied. They produced LTP with Al addition experimentally, which productivity, mechanical properties, and combustion properties were obtained. Al less than 16% and binder more than 18% were necessary to mixing and fusion molding. Regarding mentioned properties, best composition (Binder/AP/Al=18/66/16) was selected in this study.","subitem_description_type":"Other"}]},"item_5_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"},{"subitem_description":"形態: CD-ROM1枚","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"},{"subitem_description":"Note: One CD-ROM","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065073046","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10324301","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"IHIエアロスペース"},{"subitem_text_value":"IHI Aerospace (IA)"},{"subitem_text_value":"IHIエアロスペース"},{"subitem_text_value":"IHIエアロスペース"},{"subitem_text_value":"IHIエアロスペース・エンジニアリング"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace (IA)"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace (IA)"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace (IA)"},{"subitem_text_language":"en","subitem_text_value":"IHI Aerospace Engineering"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高田, 淳史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福地, 亜宝郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松浦, 新"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮川, 清"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岡本, 久夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takada, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukuchi, Aporo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuura, Shin","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyakawa, Kiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okamoto, Hisao","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"LTP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Low Melting Temperature Thermoplastic Propellant","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"次世代固体ロケット用低融点熱可塑性推進薬のアルミ添加による高性能化","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"次世代固体ロケット用低融点熱可塑性推進薬のアルミ添加による高性能化"}]},"item_type_id":"5","owner":"1","path":["1702","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16493","relation_version_is_last":true,"title":["次世代固体ロケット用低融点熱可塑性推進薬のアルミ添加による高性能化"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:52:01.069449+00:00"}