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Thrust vector control requirements for solid- propellant launch vehiclesThrust vector deflection angle requirements for controlling solid propellant launch vehicle
Document ID
19670009637
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Borsody, J. (NASA Lewis Research Center Cleveland, OH, United States)
Davidson, K. I. (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
January 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-52276
Report Number: NASA-TM-X-52276
Accession Number
67N18966
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THRUST VECTOR CONTROL /TVC/
DEFLECTION
SOLID PROPELLANT ROCKET ENGINE

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