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Flight-wind restrictions procedure, Atlas/ Centaur AC-6 through AC-15Prelaunch calculation of wind profile effect using axial load and bending moments for Atlas and Centaur launch vehicles
Document ID
19660010223
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mattson, R. T.
Date Acquired
August 3, 2013
Publication Date
May 15, 1965
Subject Category
Structural Mechanics
Report/Patent Number
GD/C-BTD-65-068
NASA-CR-54284
Report Number: GD/C-BTD-65-068
Report Number: NASA-CR-54284
Accession Number
66N19512
Funding Number(s)
CONTRACT_GRANT: NAS3-3232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CENTAUR LAUNCH VEHICLE
AXIAL LOAD
WIND PROFILE
ATLAS LAUNCH VEHICLE
BENDING MOMENT
PRELAUNCH PROBLEM

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