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Rocket Noise Prediction ProgramA comprehensive, automated, and user-friendly software program was developed to predict the noise and ignition over-pressure environment generated during the launch of a rocket. The software allows for interactive modification of various parameters affecting the generated noise environment. Predictions can be made for different launch scenarios and a variety of vehicle and launch mount configurations. Moreover, predictions can be made for both near-field and far-field locations on the ground and any position on the vehicle. Multiple engine and fuel combinations can be addressed, and duct geometry can be incorporated efficiently. Applications in structural design are addressed.
Document ID
19990040528
Acquisition Source
Kennedy Space Center
Document Type
Reprint (Version printed in journal)
Authors
Margasahayam, Ravi
(Dynacs Engineering Co., Inc. Cocoa Beach, FL United States)
Caimi, Raoul
(Dynacs Engineering Co., Inc. Cocoa Beach, FL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1999
Subject Category
Acoustics
Meeting Information
Meeting: Sound and Vibration (ICSV''6)
Location: Copenhagen
Country: Denmark
Start Date: July 5, 1999
End Date: July 8, 1999
Funding Number(s)
CONTRACT_GRANT: NAS10-98001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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