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Vibration Testing of a 1/5 Scale Model of H-II Launch Vehicle
https://jaxa.repo.nii.ac.jp/records/45320
https://jaxa.repo.nii.ac.jp/records/45320fbf56a05-60fa-4eab-9d3f-ec7bd340a9ef
名前 / ファイル | ライセンス | アクション |
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naltr01061.pdf (16.9 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 | ||||||
言語 | en | |||||
タイトル | Vibration Testing of a 1/5 Scale Model of H-II Launch Vehicle | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | H-IIロケット1/5模型の振動試験(全体試験) | |||||
著者 |
峯岸, 正勝
× 峯岸, 正勝× 佐野, 政明× 小松, 敬治× 森田, 甫之× 森野, 美樹× 富岡, 健治× 宇治野, 功× MINEGISHI, Masakatsu× SANO, Masaaki× KOMATSU, Keiji× MORITA, Toshiyuki× MORINO, Yoshiki× TOMIOKA, Kenji× UJINO, Isao |
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著者所属 | ||||||
航空宇宙技術研究所機体部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所構造力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所構造力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所構造力学部 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属(英) | ||||||
en | ||||||
Airframe Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Structural Mechanics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Structural Mechanics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Structural Mechanics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan(NASDA) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-1061 巻 1061, p. 154, 発行日 1990-04 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A 1/5 scale replica model of the H-II launch vehicle was constructed and tested for study of vehicle dynamics. This model was designed to duplicate, in miniature, as many of the full scale structural elements as was economically and technically feasible. A series of vibration tests, from the moving launcher phase to the second-stage burn-out phase, were carried out, and resonant frequencies, mode shapes, and modal dampings were measured for each case. The test data verified the mathematical modeling techniques used for predicting the vibration characteristics of the various configurations of the H-II launch vehicle. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR1061000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1061 |