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As an important load of a light satellite, the space CCD camera will endure very complicated dynamics environment when transporting and launching. In this paper, The FEM model of the CCD camera is created by MSC Patran/Nastran, then the model analysis, sinusoidal vibration and random vibration of the structure is performed. Based on the results, it proves that the CCD camera is satisfied in the ordinary condition, and this can be a reference for the similar design work.
Date of Conference: 15-17 July 2011