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II.1.9 構造の立場から見たSSRロケットの性能向上の可能性について(1 機体および構造)(II.関連研究)
https://jaxa.repo.nii.ac.jp/records/31826
https://jaxa.repo.nii.ac.jp/records/31826b6e8b863-2f23-4e11-bb69-6e9aebcd2ed6
名前 / ファイル | ライセンス | アクション |
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SA0124881.pdf (278.2 kB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | II.1.9 構造の立場から見たSSRロケットの性能向上の可能性について(1 機体および構造)(II.関連研究) | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Rossibility of Structural Improvement of SSR-Rocket | |||||
著者 |
池田, 健
× 池田, 健× 富田, 文治× 古田, 敏康× 酒巻, 正守× IKEDA, Ken× TOMITA, Bunji× FURUTA, Toshiyasu× SAKAMAKI, Masamori |
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著者所属 | ||||||
東京大学宇宙航空研究所航空力学部 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所航空力学部 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所航空力学部 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所航空力学部 | ||||||
著者所属(英) | ||||||
en | ||||||
the Institute of Space and Aeronautical Science University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
the Institute of Space and Aeronautical Science University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
the Institute of Space and Aeronautical Science University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
the Institute of Space and Aeronautical Science University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 2, 号 2_B, p. 622-626, 発行日 1966-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The small test rocket SSR, Which reached the altitude 25.8km in the latest flying test, is still possible to be improved from the structural point of view. From the results of the ground tests, the weight of some structual parts can be reduced and the reducible total weight is estimated about 30% of the total structural weight. It is shown that this weight reduction is also possible from the aeroelastic point of view. By this improvment, the increase of the maximum attainable altitude of SSR will be about 4. 7 km. Furthermore, this result is compared with the effects of aerodynamical improvement and of the improvement of the propellant. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0124881000 |