A study was made to evaluate the potential of the liquid metal lithium as a coolant for solid propellant rocket nozzles. The program plan included the analysis, design, and testing of two cooling systems: Convection; and Spray film. A literature survey was made to review the state-of-the-art of rocket nozzle cooling (Author)


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    Title :

    Cooled Solid Propellant Rocket Nozzles


    Contributors:
    S. Elkind (author)

    Publication date :

    1964


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English