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Static aerodynamic characteristics of the aborted Apollo-Saturn IB vehicleStatic aerodynamic characteristics of aborted Apollo-Saturn vehicles with normal force coefficient distributions
Document ID
19660014297
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Nunley, B. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
March 30, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-53423
Accession Number
66N23586
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SATURN IB LAUNCH VEHICLE
APOLLO SPACECRAFT
NORMAL FORCE DISTRIBUTION
STATIC AERODYNAMIC CHARACTERISTICS
ABORT

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