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Development of a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final reportThermal barrier coating for use on water cooled nozzle of solid propellant rocket engine
Document ID
19690023927
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stubbs, V. R. (Aerojet-General Corp. Sacramento, CA, United States)
Date Acquired
August 5, 2013
Publication Date
May 3, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-72549
Report Number: NASA-CR-72549
Accession Number
69N33305
Funding Number(s)
CONTRACT_GRANT: NAS3-10302
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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