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.


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    Title :

    Analysis of thermal radiation heat transfer in nuclear-rocket nozzle


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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