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Performance of rocket nozzle materials with several solid propellantsErosion resistance and thermal stress cracking tests of rocket nozzle materials with solid propellants
Document ID
19660015713
Document Type
Other - NASA Technical Note (TN)
Authors
Freche, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Johnston, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Signorelli, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3428
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMAL STRESS
SOLID PROPELLANT
REFRACTORY METAL
ROCKET NOZZLE

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