Main goals for design of high-performance propulsion system using airbreathing cycle would be high engine performance to permit substantial reduction in propellant and tank weight, total system weight, and overall dimensions, compared to rocket system; performance of supersonic combustion and problems related to structural design; combustion and mixing process; theoretical and experimental data show that supersonic processes can be used efficiently in hypersonic ramjet practical in size for launch vehicles as well as hypersonic aircraft.


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    Title :

    Supersonic combustion progress


    Additional title:

    Astronautics Aeronautics


    Contributors:
    Ferri, A. (author)

    Published in:

    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English