Feasibility study of two- or three-stage horizontal takeoff launch vehicle assuming orbit delivery of one ton load with 3300 fps velocity reserve to space laboratory orbiting at 200 mi; analysis includes concept of two recoverable vehicles and discusses configuration, separation, return, and propulsion; design assumes use of conventional airports.


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    Titel :

    French concept for aerospace transporter


    Weitere Titelangaben:

    SAE -- Space Technology Conf


    Beteiligte:
    Deplante, H. (Autor:in) / Perrier, P. (Autor:in)

    Kongress:

    Proceedings of the Space Technology Conference ; 1967 Reusable



    Erscheinungsdatum :

    1967


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A French Concept for an Aerospace Transporter

    Deplante, Henri / Perrier, Pierre | SAE Technical Papers | 1967


    Aerospace transporter system

    Roy, M. | Engineering Index Backfile | 1965


    Costing the aerospace transporter

    Clegg, W.B. / Janik, K.D. | Engineering Index Backfile | 1967


    Europe studies an aerospace transporter

    Engineering Index Backfile | 1964


    French aerospace

    Bonsignore, Ezio | GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1986