WEKO3
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ロケットエンジン高信頼化設計手法の研究:動的故障モデル、限界試験結果反映の取り組み
https://jaxa.repo.nii.ac.jp/records/6001
https://jaxa.repo.nii.ac.jp/records/6001d4d632a0-5fc1-4b94-9b39-a34d315cc5b4
名前 / ファイル | ライセンス | アクション |
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49500017.pdf (1.4 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:動的故障モデル、限界試験結果反映の取り組み | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 信頼性 | |||||
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 | 宇宙推進システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 故障解析 | |||||
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 | 動的シミュレータ | |||||
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 | エンジン試験 | |||||
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 | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reliability | |||||
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 | space propulsion system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | failure analysis | |||||
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 | dynamic simulator | |||||
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 | engine test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | liquid propellant rocket engine | |||||
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: Analytical modeling and experimental investigation of failure mechanism for engine dynamic simulator | |||||
著者 |
岩崎, 文哉
× 岩崎, 文哉× 倉谷, 尚志× 青木, 宏× 吉田, 誠× 高田, 仁志× 木村, 俊哉× 長田, 敦× Iwasaki, Fumiya× Kuratani, Naoshi× Aoki, Hiroshi× Yoshida, Makoto× Takada, Hitoshi× Kimura, Toshiya× Osada, Atsushi |
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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 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 | ||||||
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 Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Kakuda Space Center, 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. 81-86, 発行日 2006-11-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the past, space propulsion systems were usually composed by accumulating the optimum design results for each component device. Therefore, 'system reliability level' was measured by long-time development tests. Recently, the new design method is required to predict 'system reliability level' at the conceptual design phase, to grasp and to optimize the distribution of 'risks and margins' because attainable 'system reliability level' strongly depends on its basic concept. This paper describes some sample approaches to measure 'system reliability level', focusing on analytical modeling of failure mechanism for rocket engine dynamic simulator. 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: AA0049500017 | |||||
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 |