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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    Titel :

    Supersonic combustion progress


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:
    Ferri, A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch