In this part, the state of the art for several propulsion system components is reviewed, and some of the important factors which must be considered during the design of a supersonic propulsion system are pointed out. The discussion will be centered around the Mach number 3 cruise airplane of part III and the multimission airplane of part II.


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    Titel :

    IV. Air-Breathing Propulsion Systems for Supersonic Aircraft


    Beteiligte:

    Kongress:

    National Meeting on the Future of Manned Military Aircraft ; 1960 ; San Diego, CA, US



    Erscheinungsdatum :

    01.10.1960


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch






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