@article{oai:jaxa.repo.nii.ac.jp:00031822,
 author = {池田, 健 and 古田, 敏康 and 酒巻, 正守 and IKEDA, Ken and FURUTA, Toshiyasu and SAKAMAKI, Masamori},
 issue = {2_B},
 journal = {東京大学宇宙航空研究所報告},
 month = {Jun},
 note = {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., 資料番号: SA0124877000},
 pages = {585--602},
 title = {II.1.5 SSRの部品強度(1 機体および構造)(II.関連研究)},
 volume = {2},
 year = {1966}
}