Stipa-Caproni tubular monoplane with cylindrical fuselage; wings are attached to sides of tube or cylinder; pilot and passenger seats are on top, engine is inside of tube, and propeller is located at front end; weight empty, 600 kg; wing span 14.3 m, length 5.9 m. See also Engineering Index 1932 p 22 and 23. (see also German translation in Schweiz Bauzeitung v 102 n 1 July 1933 p 8-9; French translation in Genie Civil v 103 n 4 July 22 1933 p 91 and English translation in Mech Eng v 55 n 10 Oct 1933 p 631-2)


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    Titel :

    Stipa-Caproni tubular monoplane


    Weitere Titelangaben:

    L'aereo-tubolare Stipa


    Beteiligte:
    Silvestri, A. (Autor:in)

    Erschienen in:

    Politecnico ; 81 , n 2


    Erscheinungsdatum :

    1933


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Italienisch


    Schlagwörter :


    Stipa-Caproni tubular monoplane

    Silvestri, A. | Engineering Index Backfile | 1933


    Stipa-Caproni tubular monoplane

    Silvestri, A. | Engineering Index Backfile | 1933


    Stipa-Caproni tubular monoplane

    Silvestri, A. | Engineering Index Backfile | 1933


    The Stipa-Caproni Monoplane

    Giacomelli, R. | Emerald Group Publishing | 1933


    Stipa Monoplane with Venturi Fuselage

    Luigi Stipa | NTRS | 1934