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LOX/エタノールガスジェネレータの高精度流量予測に関する研究
https://jaxa.repo.nii.ac.jp/records/49483
https://jaxa.repo.nii.ac.jp/records/494836e5f8fce-191e-4b14-b538-e75189746b44
名前 / ファイル | ライセンス | アクション |
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SA6000184027.pdf (733.5 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2023-05-23 | |||||
タイトル | ||||||
タイトル | LOX/エタノールガスジェネレータの高精度流量予測に関する研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Gas Generator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Throttling | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Pressure Loss | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flow Rate | |||||
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 | The Study on High-Precision Flow Rate Prediction for LOX/Ethanol Gas Generator | |||||
著者 |
奈女良, 実央
× 奈女良, 実央× 藤浦, 彰友× 中村, 祐太× 中田, 大将× 江口, 光× 内海, 政春× NAMERA, Mio× FUJIURA, Akitomo× NAKAMURA, Yuta× NAKATA, Daisuke× EGUCHI, Hikaru× UCHIUMI, Masaharu |
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著者所属 | ||||||
室蘭工業大学工学研究科 | ||||||
著者所属 | ||||||
室蘭工業大学工学研究科 | ||||||
著者所属 | ||||||
室蘭工業大学理工学部 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属 | ||||||
室蘭工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Muroran Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS) | |||||
書誌情報 |
令和4年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium FY2022 発行日 2023-01 |
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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 | 令和4年度宇宙輸送シンポジウム(2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)) , 相模原市, 神奈川県 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, describe a method of prediction for gas generator throttled combustion tests. In addition to the conventional method, the injector Cd was set small based on past test results. As a result, the LOX flow rate error at 70% throttle was improved from 10% to 1.3%. In addition, for flight operation, the propellant orifice diameter was examined for the feed-line resistance of the control valves. | |||||
著者版フラグ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA6000184027 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | STCP-2022-027 |