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Results of an experimental investigation to determine the aerodynamic loadings on three Saturn payload shapesWind tunnel tests on Saturn launch vehicle payloads for aerodynamic loadings
Document ID
19660014359
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reese, H. B. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
August 3, 2013
Publication Date
November 10, 1964
Subject Category
Aerodynamics
Report/Patent Number
TN-AE-64-16
NASA-CR-74415
Accession Number
66N23648
Funding Number(s)
CONTRACT_GRANT: NAS8-4016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PAYLOAD
SATURN LAUNCH VEHICLE
AERODYNAMIC LOAD
WIND TUNNEL

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