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Lift-Off Acoustics Prediction of Clustered Rocket Engines in the Near FieldThis slide presentation presents a method of predicting acoustics during lift-off of the clustered rocket engines in the near field. Included is a definition of the near field, and the use of deflectors and shielding. There is discussion about the use of PAD, a software system designed to calculate the acoustic levels from the lift of of clustered rocket enginee, including updates to extend the calculation to directivity, water suppression, and clustered nozzles.
Document ID
20110003588
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Vu, Bruce
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Plotkin, Ken
(Wyle Labs., Inc. Arlington, VA, United States)
Date Acquired
August 29, 2013
Publication Date
June 8, 2010
Subject Category
Acoustics
Report/Patent Number
KSC-2010-081
Report Number: KSC-2010-081
Meeting Information
Meeting: Spacecraft and Launch Vehicle Dynamic Environments Workshop
Location: El Segundo, CA
Country: United States
Start Date: June 8, 2010
End Date: June 10, 2010
Sponsors: Aerospace Corp.
Distribution Limits
Public
Copyright
Public Use Permitted.
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