Report presents mathematical model for use in designing rocket-launching stand. Predicts pressure and thermal environment, as well as thermal responses of structures to impinging rocket-exhaust plumes. Enables relatively inexperienced analyst to determine time-varying distributions and absolute levels of pressure and heat loads on structures.


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    Title :

    Pressure And Thermal Modeling Of Rocket Launches


    Contributors:

    Published in:

    Publication date :

    1995-11-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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