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A wind profile for generating control requirements for rocket vehicles using liquid-injection control systemsWind profile developed for calculation of deflection impulse for rocket with liquid injection thrust vector control
Document ID
19690004701
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Daniele, C. 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
December 8, 1968
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-1708
Report Number: NASA-TM-X-1708
Accession Number
69N14033
Funding Number(s)
CONTRACT_GRANT: 125-19-04-02-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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