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上段エンジン用液体水素ターボポンプの形態設計の試行
https://jaxa.repo.nii.ac.jp/records/38602
https://jaxa.repo.nii.ac.jp/records/38602acb5dc6e-8bcf-4e85-82ea-afa6ebdfd019
名前 / ファイル | ライセンス | アクション |
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AC1400018.pdf (2.2 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 上段エンジン用液体水素ターボポンプの形態設計の試行 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Turbopump; Morphological design; Dynamic Design; Rotor vibration | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Trial Study on Morphological Design to a Hydrogen Turbopump for Upper Stage Engine | |||||
著者 |
内海, 政春
× 内海, 政春× 島垣, 満× 平木, 博道× 四宮, 教行× Uchiumi, Masaharu× Shimagaki, Mitsuru× Hiraki, Hiromichi× Shimiya, Noriyuki |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences(JSASS) | |||||
書誌情報 |
第57回宇宙科学技術連合講演会講演集 en : Proceedings of 57th Space Sciences and Technology Conference 発行日 2013-10 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第57回宇宙科学技術連合講演会(2013年10月9日-11日. 米子コンベンションセンター(BiG SHiP)), 米子市, 鳥取県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Rotor lateral vibration on a rocket turbopump is very serious problem. In order to suppress the rotor instabilities, the newdesign method for a turbopump, so called morphological design method was proposed by JAXA. The design methodconsists of both optimization of the component layout, and optimization of shaft diameter and length of the components.Trial study on morphological design to a hydrogen turbopump for upper stage engine was conducted. Optimizationscenarios and results were presented in this paper. | |||||
権利 | ||||||
権利情報 | (C)2013 一般社団法人 日本航空宇宙学会 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1400018000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2013-4269 |