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Thrust coefficients of low-thrust nozzlesThrust coefficients of supersonic nozzles operating at low propellant flow rates
Document ID
19650027295
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Brinich, P. F. (NASA Lewis Research Center Cleveland, OH, United States)
Jack, J. R. (NASA Lewis Research Center Cleveland, OH, United States)
Spisz, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3056
Report Number: NASA-TN-D-3056
Accession Number
65N36896
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOZZLE THRUST COEFFICIENT
THRUST MEASUREMENT
SUPERSONIC NOZZLE

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