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Experimental evaluation of throat inserts in a storable-propellant rocket engineEvaluation of erosion resistant materials for throat inserts of ablative nozzle sections in storable propellant rocket engine
Document ID
19660030254
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johnston, J. R. (NASA Lewis Research Center Cleveland, OH, United States)
Plews, L. D. (NASA Lewis Research Center Cleveland, OH, United States)
Winter, J. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1266
Report Number: NASA-TM-X-1266
Accession Number
66N39544
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ABLATING MATERIAL
NOZZLE INSERT
STORABLE PROPELLANT
ROCKET ENGINE

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