WEKO3
アイテム
{"_buckets": {"deposit": "e044bda4-ab99-4b0a-8a35-64de31503561"}, "_deposit": {"created_by": 1, "id": "6243", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6243"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006243", "sets": ["1058", "1893"]}, "author_link": ["31376", "31374", "31375", "31373"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Endurance test for the injector elements of reusable LOX/LH2 engine"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-01-20", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "60", "bibliographicPageStart": "59", "bibliographicVolumeNumber": "JAXA-SP-05-010", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術"}, {"bibliographic_title": "JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "In the Institute of Space and Astronautical Science (ISAS), a flight test campaign for studying reusable space transportation system has been performed with a small vehicle having a 10 kN class LOX/LH2 propulsion system. As a part of this study, we are evaluating the injector elements of reusable engine endured various thermal impacts with the small scale test pieces and original test equipment.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049056012", "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: JAXA-SP-05-010", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構"}]}, "item_3_publisher_9": {"attribute_name": "出版者(英)", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-113X", "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": "AA11984031", "subitem_source_identifier_type": "NCID"}]}, "item_3_text_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "宇宙船の推進及び出力"}, {"subitem_text_value": "打ち上げロケット及び宇宙機"}, {"subitem_text_value": "機械工学"}]}, "item_3_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_3_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: SP"}]}, "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: 7"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部 技術開発部"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部 宇宙輸送工学研究系"}]}, "item_3_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Technology Development Department, Institute of Space and Astronautical Science"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Dept. of Space Transportation Eng., Inst. of Space and Astronautical Science"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "八木下, 剛"}], "nameIdentifiers": [{"nameIdentifier": "31373", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "徳留, 真一郎"}], "nameIdentifiers": [{"nameIdentifier": "31374", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Yagishita, Tsuyoshi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31375", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tokudome, Shinichiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "31376", "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": "49056012.pdf", "filesize": [{"value": "854.5 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 854500.0, "url": {"label": "49056012.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6243/files/49056012.pdf"}, "version_id": "85f1aa87-427b-418d-8c19-02274f268c2a"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "宇宙輸送システム", "subitem_subject_scheme": "Other"}, {"subitem_subject": "再使用型ロケットエンジン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "燃料噴射", "subitem_subject_scheme": "Other"}, {"subitem_subject": "噴射器", "subitem_subject_scheme": "Other"}, {"subitem_subject": "耐久性試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "液体燃料ロケットエンジン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "液体水素", "subitem_subject_scheme": "Other"}, {"subitem_subject": "液体酸素", "subitem_subject_scheme": "Other"}, {"subitem_subject": "残留応力", "subitem_subject_scheme": "Other"}, {"subitem_subject": "熱衝撃サイクル", "subitem_subject_scheme": "Other"}, {"subitem_subject": "space transportation system", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "reusable rocket engine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "fuel injection", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "injector", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "endurance test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "liquid propellant rocket engine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "liquid hydrogen", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "liquid oxygen", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "residual stress", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "heat shock cycle", "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": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "液体酸素/液体水素エンジン噴射器の耐久性評価試験", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "液体酸素/液体水素エンジン噴射器の耐久性評価試験"}]}, "item_type_id": "3", "owner": "1", "path": ["1058", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6243", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6243", "relation": {}, "relation_version_is_last": true, "title": ["液体酸素/液体水素エンジン噴射器の耐久性評価試験"], "weko_shared_id": -1}
液体酸素/液体水素エンジン噴射器の耐久性評価試験
https://jaxa.repo.nii.ac.jp/records/6243
https://jaxa.repo.nii.ac.jp/records/62431345f93a-90f4-4e6f-a612-abd470935ebc
名前 / ファイル | ライセンス | アクション |
---|---|---|
49056012.pdf (854.5 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 | 液体酸素/液体水素エンジン噴射器の耐久性評価試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙輸送システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用型ロケットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料噴射 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 噴射器 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 耐久性試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 液体燃料ロケットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 液体水素 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 液体酸素 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 残留応力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱衝撃サイクル | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | space transportation system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reusable rocket engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel injection | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | injector | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | endurance test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | liquid propellant rocket engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | liquid hydrogen | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | liquid oxygen | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | residual stress | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat shock cycle | |||||
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 | Endurance test for the injector elements of reusable LOX/LH2 engine | |||||
著者 |
八木下, 剛
× 八木下, 剛× 徳留, 真一郎× Yagishita, Tsuyoshi× Tokudome, Shinichiro |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 技術開発部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙輸送工学研究系 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Technology Development Department, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Dept. of Space Transportation Eng., Inst. of Space and Astronautical Science | ||||||
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: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 en : JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems 巻 JAXA-SP-05-010, p. 59-60, 発行日 2006-01-20 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the Institute of Space and Astronautical Science (ISAS), a flight test campaign for studying reusable space transportation system has been performed with a small vehicle having a 10 kN class LOX/LH2 propulsion system. As a part of this study, we are evaluating the injector elements of reusable engine endured various thermal impacts with the small scale test pieces and original test equipment. | |||||
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: AA0049056012 | |||||
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-05-010 |