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II.5.1 飛しょう性能(5 性能および気道)(II.関連研究)
https://jaxa.repo.nii.ac.jp/records/31845
https://jaxa.repo.nii.ac.jp/records/3184559234cf1-3683-4d9e-bab5-8e8e581ce8b9
名前 / ファイル | ライセンス | アクション |
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SA0124900.pdf (344.7 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.5.1 飛しょう性能(5 性能および気道)(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 | Flight Performance of SSR Rocket | |||||
著者 |
富田, 文治
× 富田, 文治× 小早川, 眞也× 酒井, 春雄× TOMITA, Bunji× KOBAYAKAWA, Shinya× SAKAI, Haruo |
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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 | ||||||
三菱重工業K.K.名古屋航空機製作所 | ||||||
著者所属 | ||||||
三菱重工業K.K.名古屋航空機製作所 | ||||||
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. 818-825, 発行日 1966-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this report, the flight performances of SSR Rockets, HT-110-1, 2 and 3, under the condition of no cross wind are analysed. These three rockets have slightly different characteristics in total weight, configuration and weight of payload except the engine performance. The calculational results show that the maximum altitudes of trajectories of these rockets are about 20~27km when the launching angle is 70°, and that fairly good coincidence with the results of flight testing, hence especially the adequancy of evaluation of drag coefficients, which will be considered mainly to affect the performance of small rockets such as HT-110 types, was corroborated. | |||||
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: SA0124900000 |