WEKO3
アイテム
{"_buckets": {"deposit": "7a5379da-6221-47a2-ae66-a2b8101daca3"}, "_deposit": {"created_by": 1, "id": "5438", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "5438"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00005438", "sets": ["965", "1891"]}, "author_link": ["26381", "26380"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "System design of supersonic experimental airplane system"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2009-02-27", "bibliographicIssueDateType": "Issued"}, "bibliographicVolumeNumber": "JAXA-SP-08-008", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告"}, {"bibliographic_title": "JAXA Special Publication", "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": "小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館)", "subitem_description_type": "Other"}]}, "item_5_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "One of the goals of the flight test with the Supersonic Experimental Airplane (NEXST-1) is to substantiate supersonic drag reduction technology with a CFD-based optimum aerodynamic design procedure. Another goal is to establish experimental flight test technology with unmanned airplane. The second flight testing of the NEXST-1 has been successfully conducted on 10 October, 2005 at Woomera Test Range, Woomera Prohibited Area, South Australia. In this report, overview of the experimental system and design and the substantiation for system requirements from flight test data are reported.", "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"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0064239002", "subitem_description_type": "Other"}]}, "item_5_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: JAXA-SP-08-008", "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"}]}, "item_5_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_5_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-113X", "subitem_source_identifier_type": "ISSN"}]}, "item_5_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA11984031", "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: 特別資料"}]}, "item_5_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "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": "宇宙航空研究開発機構航空プログラムグループ運航・安全技術チーム"}]}, "item_5_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Operation and Safety Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "町田, 茂"}], "nameIdentifiers": [{"nameIdentifier": "26380", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Machida, Shigeru", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "26381", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "ファイル情報", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-01-16"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "64239002.pdf", "filesize": [{"value": "4.7 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 4700000.0, "url": {"label": "64239002.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/5438/files/64239002.pdf"}, "version_id": "b34a07b2-2750-49f7-b2e4-bacf4f8d17c1"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "Design, Flight Testing, Supersonic Transport, Experimental System, Unmanned airplane", "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": "ロケット実験機の飛行実験技術", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "ロケット実験機の飛行実験技術"}]}, "item_type_id": "5", "owner": "1", "path": ["965", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/5438", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "5438", "relation": {}, "relation_version_is_last": true, "title": ["ロケット実験機の飛行実験技術"], "weko_shared_id": -1}
ロケット実験機の飛行実験技術
https://jaxa.repo.nii.ac.jp/records/5438
https://jaxa.repo.nii.ac.jp/records/54380da67df9-f673-49e8-aac8-82957d5a1d39
名前 / ファイル | ライセンス | アクション |
---|---|---|
64239002.pdf (4.7 MB)
|
|
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 | ロケット実験機の飛行実験技術 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Design, Flight Testing, Supersonic Transport, Experimental System, Unmanned airplane | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | System design of supersonic experimental airplane system | |||||
著者 |
町田, 茂
× 町田, 茂× Machida, Shigeru |
|||||
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運航・安全技術チーム | ||||||
著者所属(英) | ||||||
en | ||||||
Operation and Safety Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告 en : JAXA Special Publication 巻 JAXA-SP-08-008, 発行日 2009-02-27 |
|||||
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 | 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | One of the goals of the flight test with the Supersonic Experimental Airplane (NEXST-1) is to substantiate supersonic drag reduction technology with a CFD-based optimum aerodynamic design procedure. Another goal is to establish experimental flight test technology with unmanned airplane. The second flight testing of the NEXST-1 has been successfully conducted on 10 October, 2005 at Woomera Test Range, Woomera Prohibited Area, South Australia. In this report, overview of the experimental system and design and the substantiation for system requirements from flight test data are reported. | |||||
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 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064239002 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-08-008 |