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    Title :

    Use of Discontinuous Exit Flows to Reduce Rocket Nozzle Length



    Conference:

    30th Joint propulsion conference ; 1994 ; Indianapolis; IN



    Publication date :

    1994-01-01


    Size :

    ALL


    Remarks:

    Separate paper nos AIAA 94-2700 to 94-3398 with gaps held only


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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