The durability of the SSME turbine is strongly affected by the temperature profile leaving the preburner. A reacting flow computer model to predict the turbine inlet temperature profile was used. Calculations were made by using a reacting flow code, to assess the sensitivity of the turbine inlet temperature profile to variations in the flow entering the SSME preburner.


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    Title :

    SSME Fuel Preburner Two-Dimensional Analysis


    Contributors:

    Conference:

    Structural Integrity and Durability of Reusable Space Propulsion Systems ; 1985 ; Cleveland, Ohio, US



    Publication date :

    1985-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






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