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Thrust Chamber Thermal Barrier Coating TechniquesMethods for applying thermal barrier coatings to the hot-gas side wall of rocket thrust chambers in order to significantly reduce the heat transfer in high heat flux regions has been the focus of technology efforts for many years. A successful technique developed by NASA-Lewis that starts with the coating on a mandrel and then builds the thrust chamber around it by electroforming appropriate materials is described. This results in a smooth coating with exceptional adherence, as was demonstrated in hot fire rig tests. The low cycle fatigue life of chambers with coatings applied in this manner was increased dramatically compared to uncoated chambers.
Document ID
19890013300
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Richard J Quentmeyer
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Publication Information
Publication: AGARD, Application of Advanced Material for Turbomachinery and Rocket Propulsion
Subject Category
Nonmetallic Materials
Report/Patent Number
AGARD-CP-449
Meeting Information
Meeting: 72nd Annual Specialists' Meeting
Location: Bath
Country: GB
Start Date: October 3, 1988
End Date: October 5, 1988
Sponsors: North Atlantic Treaty Organization
Accession Number
89N22671
Distribution Limits
Public
Copyright
Other
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