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Lift-Off Acoustics Predictions for the Ares I Launch PadThe vibroacoustic environment associated with large launch vehicles is of concern for the integrity of the launch complex and the vehicle itself. A large body of knowledge of this environment was developed during the early years of the missile and space flight, particularly during the Apollo program. Reference 1, prepared by Sutherland and others during that era, contains much of that knowledge. A specific process for predicting noise on and around the vehicle itself and the launcher is presented in Reference 2, prepared by Eldred, et al. Recent reviews of the process, e.g., Reference 3, have suggested some revised details but generally support the methodology in Reference 2.
Document ID
20120003611
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Kenneth J Plotkin
(Wyle (United States) El Segundo, California, United States)
Louis C Sutherland
(LCS Acoustics Rancho Palos Verdes, California, United States)
Bruce T Vu
(Kennedy Space Center Merritt Island, Florida, United States)
Date Acquired
August 25, 2013
Publication Date
May 11, 2009
Publication Information
Publication: 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference)
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781600869679
Subject Category
Acoustics
Report/Patent Number
KSC-2008-261
AIAA-2009-3163
Report Number: KSC-2008-261
Meeting Information
Meeting: 30th AIAA Aeroacoustics Conference
Location: Miami, FL
Country: US
Start Date: May 11, 2009
End Date: May 13, 2009
Sponsors: American Institute of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Launch Pad
Acoustic Sounding
Launch Vehicles
Apollo Program
Chemical Rocket
Overall Sound Pressure Level
Jet Noise
Specific Heat
Rocket Exhaust
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