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Title: Vibroacoustic analysis and experimental validation of the structural responses of NASA Mars Exploration Rover spacecraft due to acoustic launch load
Authors: Hwang, H. J.
Issue Date: 23-Jun-2003
Citation: Noise Conference 2003
Cleveland, OH, USA
Abstract: Structural responses of a spacecraft during liftoff are dominated by the intense acoustic pressure field imping on the exterior of the launch vehicle. Statistical Energy Analysis model of the NASA Mars Exploration Rover spacecraft has been developed and the SEA model was analyzed to predict vibroacoustic responses of the spacecraft under the diffuse acoustic loading condition.
Appears in Collections:JPL TRS 1992+

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