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Experimental evaluation of several ablative materials as nozzle sections of a storable- propellant rocket engineAblative material evaluation for nozzle sections of storable propellant rocket engine
Document ID
19660014266
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Meyer, C. L. (NASA Lewis Research Center Cleveland, OH, United States)
Peterson, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-TM-X-1223
Accession Number
66N23555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
ABLATING MATERIAL
ROCKET ENGINE

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