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thermal conditions during typical boost trajectoryAerodynamic heating calculation of Atlas Centaur launch vehicle trajectory
Document ID
19650010305
Document Type
Other
Authors
Roudebush, W. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
THERMODYNAMICS AND COMBUSTION
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY
ATLAS CENTAUR LAUNCH VEHICLE
AERODYNAMIC HEATING

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