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Vortex flow and erosion in rocket nozzles due to warm-gas injection for thrust vector controlVortex flow and erosion in rocket nozzles from warm-gas injection for thrust vector control
Document ID
19660007258
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Smith, G. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3241
Report Number: NASA-TN-D-3241
Accession Number
66N16547
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THRUST VECTOR CONTROL /TVC/
GAS INJECTION
ROCKET NOZZLE

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