A complete description of the liquid cooled rocket nozzle analysis program (E25107) is presented, including a users manual, program listing, and a sample problem. The program is recommended for use in designing liquid cooled rocket nozzles. In addition, it is adaptable to any system in which a liquid-cooled tubular structure is used to contain and direct the flow of a hot gas.


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    Title :

    Rocket nozzle coolant channel thermal analysis program (E25107)


    Contributors:

    Publication date :

    1972-04-14


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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