Airframe Division, National Aerospace Laboratory(NAL)
Structural Mechanics Division, National Aerospace Laboratory(NAL)
Structural Mechanics Division, National Aerospace Laboratory(NAL)
Structural Mechanics Division, National Aerospace Laboratory(NAL)
National Space Development Agency of Japan(NASDA)
National Space Development Agency of Japan(NASDA)
National Space Development Agency of Japan(NASDA)
出版者
航空宇宙技術研究所
出版者(英)
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所報告
雑誌名(英)
Technical Report of National Aerospace Laboratory TR-1061
巻
1061
ページ
154
発行年
1990-04
抄録(英)
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.