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Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flightThrust vector deflection stability analysis for minimum control requirements of booster vehicles during atmospheric flight
Document ID
19680014937
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Borsody, J. (NASA Lewis Research Center Cleveland, OH, United States)
Teren, F. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1968
Subject Category
Navigation
Report/Patent Number
NASA-TN-D-4593
Report Number: NASA-TN-D-4593
Accession Number
68N24409
Funding Number(s)
CONTRACT_GRANT: 125-17-05-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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