the Institute of Space and Aeronautical Science University of Tokyo
the Institute of Space and Aeronautical Science University of Tokyo
the Institute of Space and Aeronautical Science University of Tokyo
出版者
東京大学宇宙航空研究所
雑誌名
東京大学宇宙航空研究所報告
巻
2
号
2_B
ページ
585 - 602
発行年
1966-06
抄録（英）
This report describes the details of the fundamental testing and the strength test of the actual recket body. The contents are a) Calculation of the bending strength and stiffness of the rocket body, b) Measurement of stress and stiffness of the bending of the rocket body, c) Strength of the motor cylinder and its forehead structure subjected by the internal pressure, d) Strength of the nose cone, e) Strength of the tail surfaces and its shraud. f) Calculation of the aeroelastic critical speed of the rocket body.
II.1.5 SSRの部品強度(1 機体および構造)(II.関連研究)
SA0124877.pdf
(1.15MB)
