Experimentally determined heat transfer data obtained on JP-4 and RFNA fuels under conditions simulating those occurring during thrust chamber operation; heat flux and temperature distribution within walls of tubular chamber cooled with JP-4 and within walls of drilled passage thrust chamber cooled with RFNA are obtained.


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    Title :

    Analysis of regenerative cooling in rocket thrust chambers


    Additional title:

    Jet Propulsion


    Contributors:
    Dean, L.E. (author) / Shurley, L.A. (author)

    Published in:

    Jet Propulsion ; 28 , n 2


    Publication date :

    1958


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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