Calculation procedure for determining radiant heat flux and results of calculations of heat flux for wide range of nozzle geometries, reactor face temperatures and emissivities, and nozzle wall temperatures and emissivities; approximate method for obtaining radiant heat flux distribution for similar nozzles by relatively simple interpolation procedure was also developed.
Analysis of thermal radiation heat transfer in nuclear-rocket nozzle
NASA -- Tech Note
1961
24 pages
Report
English
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Analysis of nuclear-rocket nozzle cooling
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