{"created":"2023-06-20T15:09:19.008822+00:00","id":38829,"links":{},"metadata":{"_buckets":{"deposit":"756f45cb-038b-4ac7-bd01-5ce2785eeb4d"},"_deposit":{"created_by":1,"id":"38829","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38829"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038829","sets":["1887:1891"]},"author_link":["437103","437104","437102","437100","437099","437101"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of the aerodynamic stability of a capsule shaped model with a ballistic range"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"17","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム"},{"bibliographic_title":"JSASS Northern Branch 2016 Annual Meeting and the 17th Symposiun on Propulsion System for Reusable Launch Vehicles","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":"日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム（2016年3月9日-10日. 北海道大学大学院工学研究院), 札幌市, 北海道","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A data reduction sceme was developed to evaluate aerodynamic stability of reentry capsule shaped projectiles under subsonic free-flight condition. The final goal of the work was to obtain benchmarks of stability characteristics to compare with wind tunnel test results or CFD calculations. A free-flight test campaign was conducted with an air driven single-stage gas gun in JAXA Kakuda Space Center. In the test campaign, a capsule shaped projectile of 380g mass and of 90 mm diameter launched at flight speed 110m/s. During 52meter free-flight, pitching motion of the projectile was measured with an onboard miniature data-logger and piezoelectric accelerometers in the projectile. Damping factor during free-flight was successfully obtained through the developed data reduction scheme. Nevertheless, aerodynamic stability of this projectile has not be determined due to lack of test data.","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: AC1600098000","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会北部支部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Northern Branch of the Japan Society for Aeronautical and Space Sciences"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA12621350","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC)"},{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター(JAXA)(KSPC)"},{"subitem_text_value":"東北大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"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":"Tohoku University"}]},"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":"丹野, 英幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小室., 智幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永井, 大樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanno, Hideyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Komuro, Tomoyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagai, Daiki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Free-flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamic instability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Ballistic range","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":"バリスティックレンジを用いたカプセル形状模型空力安定評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"バリスティックレンジを用いたカプセル形状模型空力安定評価"}]},"item_type_id":"5","owner":"1","path":["1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-09-21"},"publish_date":"2016-09-21","publish_status":"0","recid":"38829","relation_version_is_last":true,"title":["バリスティックレンジを用いたカプセル形状模型空力安定評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:34:56.537018+00:00"}