WEKO3
アイテム
{"_buckets": {"deposit": "018701bb-70a5-43a6-aa07-8aed99c15d82"}, "_deposit": {"created_by": 1, "id": "14702", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "14702"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00014702", "sets": ["1670", "1891"]}, "author_link": ["134238", "134240", "134242", "134243", "134239", "134241"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Conceptual design of a two stage reusable rocket"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2003-03", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "58", "bibliographicPageStart": "55", "bibliographic_titles": [{"bibliographic_title": "宇宙航行の力学シンポジウム 平成14年度"}, {"bibliographic_title": "Symposium on Flight Mechanics and Astrodynamics 2002", "bibliographic_titleLang": "en"}]}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0045913015", "subitem_description_type": "Other"}]}, "item_5_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙科学研究所"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "The Institute of Space and Astronautical Science (ISAS)"}]}, "item_5_text_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "航空力学"}, {"subitem_text_value": "流体力学及び熱伝導"}, {"subitem_text_value": "数値解析"}]}, "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: 010"}]}, "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": "東北大学 大学院工学研究科"}, {"subitem_text_value": "東北大学 工学部"}, {"subitem_text_value": "東北大学流体科学研究所"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Tohoku University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Tohoku University Faculty of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Fluid Science, 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": "岩田, 創"}], "nameIdentifiers": [{"nameIdentifier": "134238", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "澤田, 恵介"}], "nameIdentifiers": [{"nameIdentifier": "134239", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "上條, 謙二郎"}], "nameIdentifiers": [{"nameIdentifier": "134240", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Iwata, Takumi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134241", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sawada, Keisuke", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134242", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kamijo, Kenjiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "134243", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "2段式再使用ロケット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "垂直離陸", "subitem_subject_scheme": "Other"}, {"subitem_subject": "VATOL航空機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "SSTO機", "subitem_subject_scheme": "Other"}, {"subitem_subject": "概念設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "フライバック", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ペイロード", "subitem_subject_scheme": "Other"}, {"subitem_subject": "LEO", "subitem_subject_scheme": "Other"}, {"subitem_subject": "仰角", "subitem_subject_scheme": "Other"}, {"subitem_subject": "研究開発", "subitem_subject_scheme": "Other"}, {"subitem_subject": "宇宙輸送", "subitem_subject_scheme": "Other"}, {"subitem_subject": "two-stage reusable rocket", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "vertical takeoff", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "VATOL aircraft", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "SSTO vehicle", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "conceptual design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "flying-back", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "payload", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "LEO", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "angle of attack", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "research and development", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "space transportation", "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": "2段式再使用ロケットの概念設計", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "2段式再使用ロケットの概念設計"}]}, "item_type_id": "5", "owner": "1", "path": ["1670", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/14702", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "14702", "relation": {}, "relation_version_is_last": true, "title": ["2段式再使用ロケットの概念設計"], "weko_shared_id": -1}
2段式再使用ロケットの概念設計
https://jaxa.repo.nii.ac.jp/records/14702
https://jaxa.repo.nii.ac.jp/records/147029e753e60-ba3b-41bf-ab8d-f7477df815e9
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 | 2段式再使用ロケットの概念設計 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2段式再使用ロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 垂直離陸 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | VATOL航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SSTO機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 概念設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フライバック | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ペイロード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | LEO | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 仰角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙輸送 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two-stage reusable rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | vertical takeoff | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | VATOL aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SSTO vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | conceptual design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flying-back | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | payload | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | LEO | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angle of attack | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space transportation | |||||
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 | Conceptual design of a two stage reusable rocket | |||||
著者 |
岩田, 創
× 岩田, 創× 澤田, 恵介× 上條, 謙二郎× Iwata, Takumi× Sawada, Keisuke× Kamijo, Kenjiro |
|||||
著者所属 | ||||||
東北大学 大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学 工学部 | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
宇宙航行の力学シンポジウム 平成14年度 en : Symposium on Flight Mechanics and Astrodynamics 2002 p. 55-58, 発行日 2003-03 |
|||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045913015 |