It is shown that improvement of rocket systems is possible through air augmentation of rocket thrust; rocket gases contain large amount of unburned fuel which can be burned to produce additional thrust if air is mixed into supersonic rocket exhaust; problems to be solved are development of method of mixing air with propellant gases and development of inlet; basic features of hypersonic ramjets and performance potential; problem areas relating to supersonic combustion and inlet nozzles, and engine configuration.


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    Titel :

    Hypersonic airbreathing propulsion


    Weitere Titelangaben:

    Astronautics Aeronautics


    Beteiligte:
    Avery, W.H. (Autor:in) / Dugger, G.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :