WEKO3
アイテム
{"_buckets": {"deposit": "3360c6ec-ec5e-46ff-a5f7-4e9d8e7c37d9"}, "_deposit": {"created_by": 1, "id": "32512", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "32512"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00032512", "sets": ["1890", "1910"]}, "author_link": ["409620", "409621", "409623", "409616", "409619", "409622", "409618", "409624", "409617", "409615"], "item_9_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "An Experimental Study on Liquid Hydrogen/Oxygen Turbopump: Part I. Pump"}]}, "item_9_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "1979-11", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "4", "bibliographicPageEnd": "819", "bibliographicPageStart": "787", "bibliographicVolumeNumber": "15", "bibliographic_titles": [{"bibliographic_title": "東京大学宇宙航空研究所報告"}]}]}, "item_9_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "The tests were conducted to assess the performance characteristics of a turbopump for a liquid-hydrogen, liquid-oxygen rocket engine of 7000 kg-thrust level. The general design and the production of turbo-pump had been performed in 1975 and 1976 fiscal year respectively, and then since August of 1977, 10 running tests were carried out in Noshiro Testing Center of ISAS. Data were obtained enough to estimate the performance characteristics of pumps, and then the results almost satisfies the goal intended in design. Although the trubopump presented here is designed as a flight-type, the pumps were tested first to assess their performance characteristics by means that the turbines to drive pumps were driven by nitrogen or hydrogen gas at room temperature in place of combustion gas. Both liquid-hydrogen and liquid-oxygen pumps are a single stage centirfugal-flow type with helical inducer. The report about the turbine is to be published after hot running tests using a combustion gas generator.", "subitem_description_type": "Other"}]}, "item_9_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: SA0125801000", "subitem_description_type": "Other"}]}, "item_9_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "東京大学宇宙航空研究所"}]}, "item_9_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0563-8100", "subitem_source_identifier_type": "ISSN"}]}, "item_9_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AN00161914", "subitem_source_identifier_type": "NCID"}]}, "item_9_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: ISASNII"}]}, "item_9_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 宇宙科学研究所"}]}, "item_9_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: 6"}]}, "item_9_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}, {"subitem_text_value": "東京大学宇宙航空研究所"}]}, "item_9_text_7": {"attribute_name": "著者所属(英)", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}, {"subitem_text_language": "en", "subitem_text_value": "Institute of Space and Aeronautical Science, University of Tokyo"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "棚次, 亘弘"}], "nameIdentifiers": [{"nameIdentifier": "409615", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "成尾, 芳博"}], "nameIdentifiers": [{"nameIdentifier": "409616", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "長友, 信人"}], "nameIdentifiers": [{"nameIdentifier": "409617", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "秋葉, 鐐二郎"}], "nameIdentifiers": [{"nameIdentifier": "409618", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "倉谷, 健治"}], "nameIdentifiers": [{"nameIdentifier": "409619", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "TANATSUGU, Nobuhiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409620", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NARUO, Yoshihiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409621", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NAGATOMO, Makoto", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409622", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "AKIBA, Ryojiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409623", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "KURATANI, Kenji", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "409624", "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": "2020-01-24"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "SA0125801.pdf", "filesize": [{"value": "1.6 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1600000.0, "url": {"label": "SA0125801.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/32512/files/SA0125801.pdf"}, "version_id": "1248f039-0744-40a0-a5ee-2e2e8f456c19"}]}, "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": "departmental bulletin paper", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "\u003c論文\u003e液水/液酸ターボポンプの実験 I. ポンプ", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "\u003c論文\u003e液水/液酸ターボポンプの実験 I. ポンプ"}]}, "item_type_id": "9", "owner": "1", "path": ["1890", "1910"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/32512", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "32512", "relation": {}, "relation_version_is_last": true, "title": ["\u003c論文\u003e液水/液酸ターボポンプの実験 I. ポンプ"], "weko_shared_id": -1}
<論文>液水/液酸ターボポンプの実験 I. ポンプ
https://jaxa.repo.nii.ac.jp/records/32512
https://jaxa.repo.nii.ac.jp/records/325120d3b2371-c0a8-42d0-8c8e-b9454eceb25e
名前 / ファイル | ライセンス | アクション |
---|---|---|
SA0125801.pdf (1.6 MB)
|
|
Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | <論文>液水/液酸ターボポンプの実験 I. ポンプ | |||||
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_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | An Experimental Study on Liquid Hydrogen/Oxygen Turbopump: Part I. Pump | |||||
著者 |
棚次, 亘弘
× 棚次, 亘弘× 成尾, 芳博× 長友, 信人× 秋葉, 鐐二郎× 倉谷, 健治× TANATSUGU, Nobuhiro× NARUO, Yoshihiro× NAGATOMO, Makoto× AKIBA, Ryojiro× KURATANI, Kenji |
|||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 15, 号 4, p. 787-819, 発行日 1979-11 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The tests were conducted to assess the performance characteristics of a turbopump for a liquid-hydrogen, liquid-oxygen rocket engine of 7000 kg-thrust level. The general design and the production of turbo-pump had been performed in 1975 and 1976 fiscal year respectively, and then since August of 1977, 10 running tests were carried out in Noshiro Testing Center of ISAS. Data were obtained enough to estimate the performance characteristics of pumps, and then the results almost satisfies the goal intended in design. Although the trubopump presented here is designed as a flight-type, the pumps were tested first to assess their performance characteristics by means that the turbines to drive pumps were driven by nitrogen or hydrogen gas at room temperature in place of combustion gas. Both liquid-hydrogen and liquid-oxygen pumps are a single stage centirfugal-flow type with helical inducer. The report about the turbine is to be published after hot running tests using a combustion gas generator. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0125801000 |