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Thrust vector control requirements for launch vehicles using a 260-inch solid rocket first stageGimbaled nozzle and liquid injection thrust vector control requirements for solid rocket two stage launch vehicles
Document ID
19700003019
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Borsody, J. (NASA Lewis Research Center Cleveland, OH, United States)
Daniele, C. J. (NASA Lewis Research Center Cleveland, OH, United States)
Scalzott, L. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1969
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-1906
Accession Number
70N12323
Funding Number(s)
CONTRACT_GRANT: 128-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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