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Iridium-Coated Rhenium Combustion ChamberIridium-coated rhenium combustion chamber withstands operating temperatures up to 2,200 degrees C. Chamber designed to replace older silicide-coated combustion chamber in small rocket engine. Modified versions of newer chamber could be designed for use on Earth in gas turbines, ramjets, and scramjets.
Document ID
19940000439
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Schneider, Steven J.
(NASA Lewis Research Center, Cleveland, OH.)
Tuffias, Robert H.
(Ultramet)
Rosenberg, Sanders D.
(GenCorp.)
Date Acquired
August 16, 2013
Publication Date
August 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 8
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LEW-15519
Accession Number
94B10439
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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