NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Experimental evaluation of several advanced ablative materials as nozzle sections of a storable-propellant rocket engineRelative erosion resistance of ablative materials for nozzle sections of storable-propellant rocket engine
Document ID
19680010239
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pavli, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1559
Accession Number
68N19708
Funding Number(s)
CONTRACT_GRANT: 128-31-03-00-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available