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ロケットエンジン高信頼化設計手法の研究:概念設計品質の最適化方法.起動過渡における故障シミュレーション
https://jaxa.repo.nii.ac.jp/records/6236
https://jaxa.repo.nii.ac.jp/records/623640b5b819-e137-4ff8-951c-68ddda87a759
名前 / ファイル | ライセンス | アクション |
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49056005.pdf (2.8 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ロケットエンジン高信頼化設計手法の研究:概念設計品質の最適化方法.起動過渡における故障シミュレーション | |||||
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 | 液体推薬ロケットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロケットエンジン設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 概念設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 設計最適化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 過渡応答 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 感度分析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御弁 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 冗長性 | |||||
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 | liquid propellant rocket engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rocket engine design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | concept design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | design optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transient response | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sensitivity analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control valve | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | redundancy | |||||
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 | Integrated design methodology for highly reliable liquid rocket engine: Optimizing process of concept design quality. Failure simulation at start trangent | |||||
著者 |
青木, 宏
× 青木, 宏× 田口, 秀之× 倉谷, 尚志× 岡井, 敬一× 小島, 孝之× 長谷川, 卓也× 苅田, 丈士× Aoki, Hiroshi× Taguchi, Hideyuki× Kuratani, Naoshi× Okai, Keiichi× Kojima, Takayuki× Hasegawa, Takuya× Kanda, Takeshi |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
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. 25-30, 発行日 2006-01-20 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In past, the Design for Space Systems has conducted accumulating the optimum design results for each device. 'System Reliability Level' was measured as the results of long time development tests. Recently, the new design method is required. It is necessary to predict 'System Reliability Level' at Concept Design Phase, to grasp the distribution of 'Risks and Margins', to control 'Total Reliability Level' and to optimize 'Risk Distribution' because 'Attained Reliability Level depends on its basic Concept' consequently. This paper describes the results of study to measure 'Design Quality' unifying 'FMEA', 'FMECA', 'PRA', 'PDA' and 'Simulation Tools'. Some design parameters are picked up to understand where and how their dispersion makes an effect in the whole systems and to control the total system robustness. | |||||
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: AA0049056005 | |||||
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 |