NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Rocket Launch-Induced Vibration and Ignition Overpressure ResponseRocket-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.
Document ID
20010038008
Acquisition Source
Kennedy Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Caimi, Raoul E. (NASA Kennedy Space Center Cocoa Beach, FL United States)
Margashayam, Ravi N. (DYNACS Engineering Co., Inc. Cocoa Beach, FL United States)
Nayfeh, Jamal F. (University of Central Florida Orlando, FL United States)
Thompson, Karen
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: ICSV8 International Congress on Sound and Vibration
Country: Hong Kong
Start Date: July 2, 2001
End Date: July 6, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available