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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    Titel :

    SSME Fuel Preburner Two-Dimensional Analysis


    Beteiligte:

    Kongress:

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



    Erscheinungsdatum :

    01.05.1985


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






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