Assuming the delivery with an excess velocity reserve 3.300 ft/sec of a 1 ton. transferable load to a space laboratory orbiting at 200 S.M., the feasibility of a 2 (or 3) stages “horizontal take-off transporter” is considered.Analysis includes the concept of two recoverable vehicles and discusses the configuration, separation, return and propulsion. Design assumes that conventional airports can be used without special facilities, except LOX and LH.


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    Titel :

    A French Concept for an Aerospace Transporter


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Deplante, Henri (Autor:in) / Perrier, Pierre (Autor:in)

    Kongress:

    Space Technology Conference ; 1967



    Erscheinungsdatum :

    1967-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    French concept for aerospace transporter

    Deplante, H. / Perrier, P. | Engineering Index Backfile | 1967


    Aerospace transporter system

    Roy, M. | Engineering Index Backfile | 1965


    Costing the aerospace transporter

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


    French aerospace

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


    Europe studies an aerospace transporter

    Engineering Index Backfile | 1964