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Bending mode acceleration influence on pilot control of flexible booster dynamicsBending effects on pilot control of simulated flexible Saturn V launch vehicle
Document ID
19660012358
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kilpatrick, P. S. (M.S. THESIS)
Date Acquired
August 3, 2013
Publication Date
September 1, 1965
Subject Category
Navigation
Report/Patent Number
T-65-2
NASA-CR-70585
Report Number: T-65-2
Report Number: NASA-CR-70585
Accession Number
66N21647
Funding Number(s)
CONTRACT_GRANT: NSG-577
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SATURN V LAUNCH VEHICLE
BENDING
PILOT PERFORMANCE
FLEXIBLE BODY
ATTITUDE CONTROL
SIMULATION

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