Performance is examined of a re-usable space launcher system suitable for European development with an air-breathing first stage and rocket-propelled second stage. The merits of ram-rocket and turbo-ramjet propulsion are compared and the research programme required for such a system is discussed. It is concluded that a partly air-breathing re-usable launcher system is likely to emerge as a by-product of air transport development.


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    Titel :

    Air-Breathing Reusable Launchers


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Francis, R. H. (Autor:in)

    Kongress:

    Space Technology Conference ; 1967



    Erscheinungsdatum :

    1967-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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