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Please use this identifier to cite or link to this item: http://hdl.handle.net/2014/11593

Title: Prediction and validation of high frequency vibration repsonses of NASA Mars Pathfinder spacecraft due to acoustic launch load using statistical energy analysis
Authors: Hwang, H. J.
Issue Date: 28-Apr-2002
Citation: Institute of Environmental Sciences and Technology, ESTECH 2002 Conference
Anaheim, CA, USA
Abstract: Mid and high frequency structural responses of a spacecraft during the launch condition are mainly dominated by the intense acoustic pressure field over the exterior of the launch vehicle. The prediction of structural responses due to the acoustic launch load is therefore an important analysis for engineers and scientists to correctly define various dynamics specifications of the spacecraft.
URI: http://hdl.handle.net/2014/11593
Appears in Collections:JPL TRS 1992+

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