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Atlas base drag studyProposed changes to Atlas booster stage drag simulation method for improving agreement between predicted and actual flight data
Document ID
19660009183
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Frayer, R. G.
Date Acquired
August 3, 2013
Publication Date
June 21, 1965
Subject Category
Aerodynamics
Report/Patent Number
GD/C-BTD-65-089
NASA-CR-54501
Report Number: GD/C-BTD-65-089
Report Number: NASA-CR-54501
Accession Number
66N18472
Funding Number(s)
CONTRACT_GRANT: NAS3-3232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ASCENT TRAJECTORY
DRAG
ATLAS LAUNCH VEHICLE
FLIGHT SIMULATION

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