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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    IV. Air-Breathing Propulsion Systems for Supersonic Aircraft


    Contributors:

    Conference:

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



    Publication date :

    1960-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    SUPERSONIC AIRCRAFT PROPULSION INSTALLATION

    BRADBROOK STEPHEN J | European Patent Office | 2020

    Free access

    Supersonic aircraft propulsion installation

    European Patent Office | 2018

    Free access

    Supersonic aircraft propulsion installation

    BRADBROOK STEPHEN J | European Patent Office | 2022

    Free access