Iridium-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.
Iridium-Coated Rhenium Combustion Chamber
NASA Tech Briefs ; 18 , 8
1994-08-01
Miscellaneous
No indication
English
Iridium-Coated Rhenium Combustion Chamber
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