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Aeroelastic load growth effects on Saturn configurationsAnalytical evaluation of aerodynamic load growth or steady state aeroelastic effect for Saturn configurations
Document ID
19670025706
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Papadopoulos, J. G. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
July 14, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-53634
Accession Number
67N35035
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOAD FACTOR
AEROELASTICITY
STEADY STATE
SATURN LAUNCH VEHICLE

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