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Load relief autopilot analysis to minimize launch vehicle peak thrust vector deflection requirementsLoad relief autopilot to minimize launch vehicle thrust vector deflection angle required for vehicle stability during flight through design winds
Document ID
19680024284
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Scalzott, L. L. (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
September 1, 1968
Subject Category
Navigation
Report/Patent Number
NASA-TN-D-4786
Report Number: NASA-TN-D-4786
Accession Number
68N33756
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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