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Panel flutter studies of boost-vehicle full-scale flight insulation panelsSupersonic wind tunnel tests on flutter resistance of Centaur flight insulation panels
Document ID
19670023223
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Greene, R. L. (NASA Lewis Research Center Cleveland, OH, United States)
Nacht, M. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-1417
Report Number: NASA-TM-X-1417
Accession Number
67N32552
Funding Number(s)
CONTRACT_GRANT: 891-05-00-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT TEST
PANEL FLUTTER
SUPERSONIC WIND TUNNEL
CENTAUR LAUNCH VEHICLE

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