Review of principal issues governing feasibility of resuable launch vehicle systems, i.e., propulsion, structural weights, heat protection, and costs, is presented; dependence on flight Mach number of fuel specific impulse of airbreathing propulsion systems (turbojets, ramjets, and scramjets) is reduced to dependence on staging velocity of effective specific impulse values, including flight losses, to provide performance relations for preliminary design use; configurations of rocket and airbreathing reusable vehicles are selected and structural weights are characterized in terms of specific surface weights.


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    Titel :

    Reusable space launch vehicle concepts -- Outlook 1965


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Vaglio-Laurin, R. (Autor:in) / Finke, R.G. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 Launching



    Erscheinungsdatum :

    1965


    Format / Umfang :

    17 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Reusable Space Launch Vehicle Concepts: Outlook 1965

    Finke, Reinald G. / Vaglio-Laurin, Roberto | SAE Technical Papers | 1965


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    Online Contents | 2009


    Reusable Launch Vehicles Outlook

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