{"created":"2023-06-20T14:35:38.919660+00:00","id":1904,"links":{},"metadata":{"_buckets":{"deposit":"947fa217-c72c-4880-bfbf-1b75b1f29a09"},"_deposit":{"created_by":1,"id":"1904","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"1904"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00001904","sets":["1398:1421:1425","1887:1893","9:10:54:58"]},"author_link":["1317","1314","1313","1316","1315","1318"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Burning rate control of AP composite propellants: Effects of TiO2 additive"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-03-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"59","bibliographicPageStart":"55","bibliographicVolumeNumber":"JAXA-RR-15-004","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27年度研究成果報告書"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究の目的は，固体ロケットにおける人工衛星輸送能力を左右する第3段固体ロケットモータ用固体推進薬の高性能化である。第3段用固体推進薬の高性能化には，Al粒子の集塊抑制及び低燃焼速度化が要求される。本研究では，Al粒子と異なる集塊特性を持つMg-Al粒子を用いてAl粒子の集塊抑制を検討している。しかしながら，Mg-Al系推進薬はAl系推進薬と比較して燃焼速度が高い。低燃焼速度かつAl粒子の燃焼促進を図るために，燃焼負触媒を加える手法が挙げられる。本報告では，Al系推進薬及びMg-Al系推進薬にTiO2粒子を添加し，固体推進薬の燃焼速度に対するTiO2粒子添加の効果を取得した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To improve the propulsion performance of third stage solid rocket motor, high-performance solid propellant is required. This propellant is needed to inhibit Al agglomeration on the combustion surface and decrease burning rate. In this study, Mg-Al particles are incorporated into the general solid propellants in order to reduce Al agglomeration since the agglomeration characteristics of Mg-Al are different to Al. However, the burning rate of propellants containing Mg-Al particles is higher than that containing Al. To control the burning rate solid propellants, the catalysts are generally added. In this study, the effects of titanium oxide as a catalyst to burning rate of AP composite propellants are obtained.","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: AA1530055008","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-15-004","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":"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":"総合研究大学院大学(SOKENDAI)"},{"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)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"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":"The Graduate University for Advanced Studies (SOKENDAI)"},{"subitem_text_language":"en","subitem_text_value":"Department of Space Flight Systems, 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":"松本, 幸太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 祥大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"羽生, 宏人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsumoto, Kotaro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwasaki, Akihiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Habu, Hiroto","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":"AA1530055008.pdf","filesize":[{"value":"754.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1530055008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/1904/files/AA1530055008.pdf"},"version_id":"9006458b-8781-4784-85a7-e1b70bc0dcef"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aluminum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Magnalium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Solid Propellant","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Burning Rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Titanium Oxide","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":"AP系コンポジット推進薬の燃焼速度制御: TiO2添加の効果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"AP系コンポジット推進薬の燃焼速度制御: TiO2添加の効果"}]},"item_type_id":"3","owner":"1","path":["58","1425","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-03-18"},"publish_date":"2016-03-18","publish_status":"0","recid":"1904","relation_version_is_last":true,"title":["AP系コンポジット推進薬の燃焼速度制御: TiO2添加の効果"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:32:46.306252+00:00"}