Rocket-induced vibration and ignition overpressure response environments are predicted in the low-frequency (5 to 200 hertz) range. The predictions are necessary to evaluate their impact on critical components, structures, and facilities in the immediate vicinity of the rocket launch pad.
Rocket Launch-Induced Vibration and Ignition Overpressure Response
International Congress on Sound and Vibration ; 2001 ; Hong Kong
2001-01-01
Preprint
Keine Angabe
Englisch