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Saturn V Ground Winds ProgramThe concept on Saturn V was to "budget" an amount for the dynamic portion of the wind load as a factor on the steady state drag. Wind tunnel tests paralled the development and fabrication phases. The results indicated that the system was unable to withstand the design winds; thus, a decision was made to implement a viscous damper "fix" on the facility vehicle at the Kennedy Space Center. Damping tests in the Vertical Assembly Building (VAB) will have been completed and response tests on the pad will be in progress at the time of this symposium. This paper will present the history and status of this program to date.
Document ID
19660022939
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Robert M Hunt
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Accession Number
66N32229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VISCOUS DAMPING
WIND EFFECT
SATURN V LAUNCH VEHICLE
AERODYNAMIC LOAD
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