Details of new light biplane; 103 to 105 m.p.h. top speed; wing span 28 ft. 7 in.; wing section thick; all wings are interchangeable; so is rudder with either of elevators, and vice versa; so is fin with either outer section of tailplane which is designed in three sections; all main bracing wires are of same size and length; Cirrus Mark II engine. (See also Simmonds' "Spartan." Flight vol. 20, no. 1028, Sept. 6, 1928 pp. 765-766, 5 figs; Aeroplane, vol. 35, no. 4, July 25, 1928, p. 230, 1 fig.; and Airways, vol. 5, no. 1, Sept. 1928, pp. 27 and 34, 2 figs)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Simmonds. Simmonds' "Spartan."


    Weitere Titelangaben:

    Aviation


    Erschienen in:

    Aviation ; 25 , n 9


    Erscheinungsdatum :

    1928


    Anmerkungen:

    1 Fig.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Simmonds. Simmonds' "Spartan."

    Engineering Index Backfile | 1928


    Simmonds. Simmonds' "spartan."

    Engineering Index Backfile | 1928


    Simmonds. Simmonds' "Spartan."

    Engineering Index Backfile | 1928


    Simmonds aircraft, limited

    Engineering Index Backfile | 1929


    Reply by Author to J.G. Simmonds

    RONALD L. HUSTON | AIAA | 1966