NASA NTRS · 20020002698
Rocket Launch-Induced Vibration and Ignition Overpressure Response
Abstract
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.
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Caimi, Raoul, Margasahayam, Ravi, Nayfeh, Jamal, Thompson, Karen. 2001-01-01. Rocket Launch-Induced Vibration and Ignition Overpressure Response. https://ntrs.nasa.gov/citations/20020002698
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