WEKO3
アイテム
{"_buckets": {"deposit": "a6341cd8-1a45-44b5-b9f4-533efd40130b"}, "_deposit": {"created_by": 1, "id": "43886", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "43886"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00043886", "sets": ["1893", "1916"]}, "author_link": ["466129", "466132", "466131", "466130"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Aerodynamic Performance of DAS in Free Molecular Flow"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1976-07", "bibliographicIssueDateType": "Issued"}, "bibliographicPageStart": "11", "bibliographicVolumeNumber": "303", "bibliographic_titles": [{"bibliographic_title": "航空宇宙技術研究所資料"}, {"bibliographic_title": "Technical Memorandum of National Aerospace Laboratory", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "Aerodynamic force,torque and center of pressure in a free molecular flow were calculated for angle of attack up to 45。・or several sets of DAS (Dive and Ascent Satellite) configuration parameters.The most preferable shape was was found to be one in which displacement of the center of pressure is very small.The effects of momentum accomodation coefficients on aerodynamic characteristics were also estimated.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: NALTM0303000", "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: NAL TM-303", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "航空宇宙技術研究所"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "National Aerospace Laboratory(NAL)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0452-2982", "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": "AN00314334", "subitem_source_identifier_type": "NCID"}]}, "item_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: NAL-MATCH"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 航空宇宙技術研究所"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: AP"}]}, "item_3_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: 9"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "航空宇宙技術研究所空気力学第一部"}, {"subitem_text_value": "航空宇宙技術研究所空気力学第一部"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "恩地, 瑛"}], "nameIdentifiers": [{"nameIdentifier": "466129", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "津田, 尚一"}], "nameIdentifiers": [{"nameIdentifier": "466130", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "ONJI, Akira", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "466131", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "TSUDA, Shoichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "466132", "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": "2020-01-28"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "naltm00303.pdf", "filesize": [{"value": "616.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 616900.0, "url": {"label": "naltm00303.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/43886/files/naltm00303.pdf"}, "version_id": "01b600d2-95d1-48ba-acd7-c63828978cd6"}]}, "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": "自由分子流におけるDASの空力特性", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "自由分子流におけるDASの空力特性"}]}, "item_type_id": "3", "owner": "1", "path": ["1893", "1916"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/43886", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "43886", "relation": {}, "relation_version_is_last": true, "title": ["自由分子流におけるDASの空力特性"], "weko_shared_id": -1}
自由分子流におけるDASの空力特性
https://jaxa.repo.nii.ac.jp/records/43886
https://jaxa.repo.nii.ac.jp/records/43886af6d3612-dc46-43e0-bae9-125d760c30ec
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltm00303.pdf (616.9 kB)
|
|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 自由分子流におけるDASの空力特性 | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Aerodynamic Performance of DAS in Free Molecular Flow | |||||
著者 |
恩地, 瑛
× 恩地, 瑛× 津田, 尚一× ONJI, Akira× TSUDA, Shoichi |
|||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第一部 | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 303, p. 11, 発行日 1976-07 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aerodynamic force,torque and center of pressure in a free molecular flow were calculated for angle of attack up to 45。・or several sets of DAS (Dive and Ascent Satellite) configuration parameters.The most preferable shape was was found to be one in which displacement of the center of pressure is very small.The effects of momentum accomodation coefficients on aerodynamic characteristics were also estimated. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0303000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-303 |