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COLD-AIR INVESTIGATION OF THREE VARIABLE-THROAT-AREA CONVERGENTDIVERGENT NOZZLESThrust modulation techniques - cold flow tests of three variable-throat-area convergent-divergent nozzles
Document ID
19630002674
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mc Aulay, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-42
Report Number: NASA-TM-X-42
Accession Number
63N12550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONVERGENT-DIVERGENT NOZZLE
DIVERGENT NOZZLE
ROCKET NOZZLE
VARIABLE THRUST
CONVERGENT NOZZLE
THRUST

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