WEKO3
アイテム
{"_buckets": {"deposit": "be23d154-cc97-41b1-9169-f4a07ba99868"}, "_deposit": {"created_by": 1, "id": "6008", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "6008"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00006008", "sets": ["1028", "1893"]}, "author_link": ["29857", "29854", "29852", "29858", "29849", "29856", "29853", "29855", "29851", "29850"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル(英)", "attribute_value_mlt": [{"subitem_alternative_title": "Research and development of ejector rocket for combined cycle engine: Design and production of clustered rocket chamber for combined cycle engine"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2006-11-01", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "116", "bibliographicPageStart": "111", "bibliographicVolumeNumber": "JAXA-SP-06-006", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書"}, {"bibliographic_title": "JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency", "bibliographic_titleLang": "en"}]}]}, "item_3_description_17": {"attribute_name": "抄録(英)", "attribute_value_mlt": [{"subitem_description": "A gaseous hydrogen/gaseous oxygen rocket chamber was designed to fit in a rocket-ramjet combined cycle engine model, and its performance was evaluated experimentally. Such a rocket chamber is required to operate in a very wide operation range in terms of chamber pressure (P(sub c)) and mixture ratio (O/F). For stable operation, the injector has a choking point and a diffuser in the downstream portion. The design point of the injector is P(sub c) = 5.0 MPa, O/F = 7 when the supplying pressure of fuel and oxidizer is 7 MPa. The stable operation and 0.91 of the C* efficiency was attained in the ejector-jet/rocket mode operation at O/F = 6.5-7.5 and P(sub c) = 3-5 MPa. A stable operation and 0.93 of the C* efficiency was attained in the ramjet mode operation at O/F = 4.5-7 and P(sub c) = 0.6 MPa. The number of oxygen injectors used was variable, and stable operation was attained by supplying oxygen from two, three and four of eight injectors in the scramjet mode operation. The C* efficiency was 0.94 with four oxygen injector elements at O/F = 0.89, and 0.92 with three oxygen injector elements at O/F = 0.49. No thermal damage was observed in the all operating mode with a flush face injector. Since it was confirmed that the rocket chamber and the injector was able to be operated with stability in the all operating mode, a clustered rocket chamber to embed to the combined cycle engine was fabricated in FY2005.", "subitem_description_type": "Other"}]}, "item_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0049500024", "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-06-006", "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": "航空機の推進及び動力"}, {"subitem_text_value": "宇宙船の推進及び出力"}]}, "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 総合技術研究本部 角田宇宙センター"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター"}, {"subitem_text_value": "宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター"}]}, "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 Kakuda Space Center, Institute of Aerospace Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "竹腰, 正雄"}], "nameIdentifiers": [{"nameIdentifier": "29849", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "富岡, 定毅"}], "nameIdentifiers": [{"nameIdentifier": "29850", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "植田, 修一"}], "nameIdentifiers": [{"nameIdentifier": "29851", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "齋藤, 俊仁"}], "nameIdentifiers": [{"nameIdentifier": "29852", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "泉川, 宗男"}], "nameIdentifiers": [{"nameIdentifier": "29853", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takegoshi, Masao", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "29854", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Tomioka, Sadatake", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "29855", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ueda, Shuichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "29856", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Saito, Toshihito", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "29857", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Izumikawa, Muneo", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "29858", "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": "49500024.pdf", "filesize": [{"value": "1.3 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1300000.0, "url": {"label": "49500024.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/6008/files/49500024.pdf"}, "version_id": "8f93473c-cd3c-4148-82eb-d11a01014f19"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "ロケットラムジェット複合エンジン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "エジェクタロケット", "subitem_subject_scheme": "Other"}, {"subitem_subject": "燃焼室", "subitem_subject_scheme": "Other"}, {"subitem_subject": "インジェクタ", "subitem_subject_scheme": "Other"}, {"subitem_subject": "スクラムジェットエンジン", "subitem_subject_scheme": "Other"}, {"subitem_subject": "性能試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "燃焼試験", "subitem_subject_scheme": "Other"}, {"subitem_subject": "酸素", "subitem_subject_scheme": "Other"}, {"subitem_subject": "水素", "subitem_subject_scheme": "Other"}, {"subitem_subject": "rocket-ramjet combined-cycle engine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "ejector rocket", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "combustion chamber", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "injectors", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "scramjet engine", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "performance test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "combustion test", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "oxygen", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "hydrogen", "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": "複合エンジン用エジェクターロケットの研究開発:複合エンジン組み込み用2連装ロケット燃焼器の設計・製作", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "複合エンジン用エジェクターロケットの研究開発:複合エンジン組み込み用2連装ロケット燃焼器の設計・製作"}]}, "item_type_id": "3", "owner": "1", "path": ["1028", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/6008", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "6008", "relation": {}, "relation_version_is_last": true, "title": ["複合エンジン用エジェクターロケットの研究開発:複合エンジン組み込み用2連装ロケット燃焼器の設計・製作"], "weko_shared_id": -1}
複合エンジン用エジェクターロケットの研究開発:複合エンジン組み込み用2連装ロケット燃焼器の設計・製作
https://jaxa.repo.nii.ac.jp/records/6008
https://jaxa.repo.nii.ac.jp/records/6008fda75842-76fb-48bf-9b82-2a053d22948b
名前 / ファイル | ライセンス | アクション |
---|---|---|
49500024.pdf (1.3 MB)
|
|
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 | 複合エンジン用エジェクターロケットの研究開発:複合エンジン組み込み用2連装ロケット燃焼器の設計・製作 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロケットラムジェット複合エンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エジェクタロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼室 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | インジェクタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スクラムジェットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 性能試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 酸素 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 水素 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rocket-ramjet combined-cycle engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ejector rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion chamber | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | injectors | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | scramjet engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | performance test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustion test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | oxygen | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hydrogen | |||||
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 | Research and development of ejector rocket for combined cycle engine: Design and production of clustered rocket chamber for combined cycle engine | |||||
著者 |
竹腰, 正雄
× 竹腰, 正雄× 富岡, 定毅× 植田, 修一× 齋藤, 俊仁× 泉川, 宗男× Takegoshi, Masao× Tomioka, Sadatake× Ueda, Shuichi× Saito, Toshihito× Izumikawa, Muneo |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 角田宇宙センター | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Aerospace Technology | ||||||
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18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 en : JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency 巻 JAXA-SP-06-006, p. 111-116, 発行日 2006-11-01 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A gaseous hydrogen/gaseous oxygen rocket chamber was designed to fit in a rocket-ramjet combined cycle engine model, and its performance was evaluated experimentally. Such a rocket chamber is required to operate in a very wide operation range in terms of chamber pressure (P(sub c)) and mixture ratio (O/F). For stable operation, the injector has a choking point and a diffuser in the downstream portion. The design point of the injector is P(sub c) = 5.0 MPa, O/F = 7 when the supplying pressure of fuel and oxidizer is 7 MPa. The stable operation and 0.91 of the C* efficiency was attained in the ejector-jet/rocket mode operation at O/F = 6.5-7.5 and P(sub c) = 3-5 MPa. A stable operation and 0.93 of the C* efficiency was attained in the ramjet mode operation at O/F = 4.5-7 and P(sub c) = 0.6 MPa. The number of oxygen injectors used was variable, and stable operation was attained by supplying oxygen from two, three and four of eight injectors in the scramjet mode operation. The C* efficiency was 0.94 with four oxygen injector elements at O/F = 0.89, and 0.92 with three oxygen injector elements at O/F = 0.49. No thermal damage was observed in the all operating mode with a flush face injector. Since it was confirmed that the rocket chamber and the injector was able to be operated with stability in the all operating mode, a clustered rocket chamber to embed to the combined cycle engine was fabricated in FY2005. | |||||
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: AA0049500024 | |||||
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-06-006 |