414 拡散音場及び定在波音場負荷時の宇宙機構造の振動感度に関する研究

概要

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Satellites are launched to space with locked up inside fairing which is top of rocket. When rockets are launched, mounted satellites are under inclement mechanical environment and various mixed mechanical environment act satellites. Satellites should be designed to withstand such mixed environment and are tested and estimated as each environment. In this thesis, we focus on environment of acoustic load of satellites and consider response of acoustic vibration of satellites.
一般社団法人日本機械学会の論文
2009-08-03