{"created":"2023-06-20T14:35:43.739273+00:00","id":2004,"links":{},"metadata":{"_buckets":{"deposit":"a39364de-60d0-4de6-bacc-d9fb2c3c9f03"},"_deposit":{"created_by":1,"id":"2004","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2004"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002004","sets":["1398:1421:1428","1887:1893","9:10:87:92"]},"author_link":["2211","2204","2208","2201","2203","2200","2202","2207","2210","2205","2209","2206"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-03-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"7","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-12-005","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24年度研究成果報告書"},{"bibliographic_title":"JAXA Research and Development Report: Collaborative Research Activity on Energetic Materials Research Report FY2012","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Combustion characteristics of pelletized ammonium dinitramide (ADN) and ADN-based propellants have been studied. Micron-meter-sized particles of Al, Fe2O3, TiO2, NiO, Cu(OH)NO3, Cu and CuO, and nano-meter-sized Al (Alex) and CuO (nanoCuO) were employed as the additives for pelletized ADN. Only nanoCuO and Alex show the remarkable effects, so they are also added to ADN-based propellant. The binder of ADN-based propellant is thermoplastic elastomer (TP), and three kinds of mixtures (TP:ADN = 30:70, 20:80 and 10:90 mass%) were prepared .The burning rates of pelletized ADN and ADN-based propellants were measured under the pressure range from 0.6 to 6.2 MPa, and the surface temperature profiles were obtained about ADN-based propellants. Nano-sized CuO enhanced the burning rate of pelletized ADN. Alex-incorporated ADN burned with flames even at 0.55 MPa under which pure ADN does not form the flame. Burning rate of nonadditive ADN-based propellants has extremely high pressure dependency. In the case of TP/ADN (30:7, burning rate jump are found from the critical pressure approximately 3.2MPa. The temperature profiles of TP/ADN (30:70) were measured, and the combustion　structure was discussed. Both nanoCuO and Alex improved the burning rate characteristics,　and the pressure exponents are 0.54 and 0.76 respectively.","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: AA0061907001","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-12-005","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(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":"東京大学大学院"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"細谷火工株式会社"},{"subitem_text_value":"細谷火工株式会社"},{"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":"Graduate School of the University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Hosoya Pyro-Engineering Co., Ltd."},{"subitem_text_language":"en","subitem_text_value":"Hosoya Pyro-Engineering Co., Ltd."},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Fujisato, Koji"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Habu, Hiroto"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hori, Keiichi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shibamoto, Hidefumi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yu, Xiuchao"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyake, Atsumi"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujisato, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Habu, Hiroto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hori, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shibamoto, Hidefumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yu, Xiuchao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyake, Atsumi","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":"61907001.pdf","filesize":[{"value":"664.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61907001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2004/files/61907001.pdf"},"version_id":"fd2b2444-dc8b-44c5-9eec-56955d48e451"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ADN; burning rate; surface temperature; burning rate modifier; nanoparticle","subitem_subject_scheme":"Other"},{"subitem_subject":"ADN; burning rate; surface temperature; burning rate modifier; nanoparticle","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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 wave structure of ADN based composite propellant","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Combustion wave structure of ADN based composite propellant","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["92","1428","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2004","relation_version_is_last":true,"title":["Combustion wave structure of ADN based composite propellant"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:30:39.136549+00:00"}