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.
Prediction and validation of high frequency vibration repsonses of NASA Mars Pathfinder spacecraft due to acoustic launch load using statistical energy analysis
Institute of Environmental Sciences and Technology, ESTECH 2002 Conference
2002-04-28
Conference paper
No indication
English
Mars Pathfinder Status at Launch
NTRS | 1996
|Mars Pathfinder Status at Launch
NTIS | 1996
|