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H-2A第2段ターボポンプの予冷熱解析
https://jaxa.repo.nii.ac.jp/records/2740
https://jaxa.repo.nii.ac.jp/records/274053c14a67-dd51-4481-a961-9d921ca265b9
名前 / ファイル | ライセンス | アクション |
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47944009.pdf (1.9 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 | H-2A第2段ターボポンプの予冷熱解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2Aロケット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 予冷 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ターボポンプ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱解析 | |||||
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 | 温度依存性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝導度 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H-2A rocket | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | precooling | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbopump | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal analysis | |||||
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 | temperature dependence | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal conductivity | |||||
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 | Pre-cooling analysis of the H-2A 2nd stage turbo-pumps | |||||
著者 |
遠山, 伸一
× 遠山, 伸一× 芳仲, 敏成× Toyama, Shinichi× Yoshinaka, Toshinari |
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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(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研究開発資料: 平成15年度総合技術研究本部宇宙領域研究成果報告書:輸送系 en : JAXA Research and Development Memorandum: FY15 Annual Report of Research & Development on Space Technology in the Institute of Space Technology and Aeronautics: Space Transportation System 巻 JAXA-RM-04-009, p. 43-48, 発行日 2004-10-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Before the ignition and restart of the 2nd stage engines of H-2A rocket, the turbo-pumps must be sufficiently cooled by liquid Oxygen and Hydrogen preliminary. But, the cooling duration was determined by the experimental and previous flight data. Thermal analyses have been conducted to predict the duration precisely and estimate the necessary quantities of liquid Oxygen and Hydrogen. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047944009 | |||||
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-RM-04-009 |