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Static stability and axial force characteristics of a 1.32 percent scale model of the Saturn IB/Apollo, its components, and the Saturn IB/Apollo/Minuteman launch vehicle, determined by wind tunnel testWind tunnel stability tests of scale model Saturn IB/Apollo, and Saturn IB/Apollo/ Minuteman launch vehicle
Document ID
19660014217
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chianese, F. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
August 3, 2013
Publication Date
September 9, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-74458
TN-AE-65-97
Report Number: NASA-CR-74458
Report Number: TN-AE-65-97
Accession Number
66N23506
Funding Number(s)
CONTRACT_GRANT: NAS8-4016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SATURN IB LAUNCH VEHICLE
MINUTEMAN ICBM
WIND TUNNEL STABILITY TEST
APOLLO SPACECRAFT

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