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Origin of high-intensity noise in the area of a large protuberance on a launch vehicleOrigin of high intensity noise in area of large protuberance on Atlas-Agena-Mariner C model tested in supersonic wind tunnel
Document ID
19660022060
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nacht, M. L. (NASA Lewis Research Center Cleveland, OH, United States)
Turk, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-1261
Report Number: NASA-TM-X-1261
Accession Number
66N31350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SCALE MODEL
SUPERSONIC WIND TUNNEL
ATLAS AGENA LAUNCH VEHICLE
PROTUBERANCE
NOISE INTENSITY

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