WEKO3
アイテム
{"_buckets": {"deposit": "55e2abc1-4fd9-49be-9012-9d994e20e347"}, "_deposit": {"created_by": 1, "id": "16465", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "16465"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00016465", "sets": ["1702", "1891"]}, "author_link": ["149498", "149496", "149500", "149501", "149497", "149499"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Study on Hypersonic Experimental Vehicle System Concept with an Optimal Design Method"}]}, "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": "This paper describes conceptual studies on hypersonic experimental vehicle systems. In this research, we focus on studying the hypersonic experimental systems that provides test environment for precooled turbojet. The experiment aims to acquire engine operational data during the flight at speeds over Mach 4. We conducted flight dynamics simulations at different initial conditions and optimized the trajectories.", "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: AA0065073018", "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_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: シンポジウム・研究会"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 013"}]}, "item_5_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 7"}]}, "item_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "東京大学"}, {"subitem_text_value": "東京大学"}, {"subitem_text_value": "宇宙航空研究開発機構航空プログラムグループ (JAXA)(APG)"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)(APG)"}]}, "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": "森本, 明"}], "nameIdentifiers": [{"nameIdentifier": "149496", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "土屋, 武司"}], "nameIdentifiers": [{"nameIdentifier": "149497", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "田口, 秀之"}], "nameIdentifiers": [{"nameIdentifier": "149498", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Morimoto, Akira", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "149499", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tsuchiya, Takeshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "149500", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Taguchi, Hideyuki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "149501", "nameIdentifierScheme": "WEKO"}]}]}, "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": "最適設計手法による極超音速飛行実験機システム構想の検討", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "最適設計手法による極超音速飛行実験機システム構想の検討"}]}, "item_type_id": "5", "owner": "1", "path": ["1702", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/16465", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "16465", "relation": {}, "relation_version_is_last": true, "title": ["最適設計手法による極超音速飛行実験機システム構想の検討"], "weko_shared_id": -1}
最適設計手法による極超音速飛行実験機システム構想の検討
https://jaxa.repo.nii.ac.jp/records/16465
https://jaxa.repo.nii.ac.jp/records/16465c7228391-c896-4b2a-bb5d-632b3b1d692b
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 最適設計手法による極超音速飛行実験機システム構想の検討 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Study on Hypersonic Experimental Vehicle System Concept with an Optimal Design Method | |||||
著者 |
森本, 明
× 森本, 明× 土屋, 武司× 田口, 秀之× Morimoto, Akira× Tsuchiya, Takeshi× Taguchi, Hideyuki |
|||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空プログラムグループ (JAXA)(APG) | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)(APG) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
平成22年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2010 発行日 2011 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper describes conceptual studies on hypersonic experimental vehicle systems. In this research, we focus on studying the hypersonic experimental systems that provides test environment for precooled turbojet. The experiment aims to acquire engine operational data during the flight at speeds over Mach 4. We conducted flight dynamics simulations at different initial conditions and optimized the trajectories. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065073018 |