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.; also Aviation, vol. 25, no. 9, Aug. 25, 1928, p. 606, 1 fig.)


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    Title :

    Simmonds. Simmonds' "Spartan."


    Additional title:

    Airways


    Published in:

    Airways ; 5 , n 1


    Publication date :

    1928


    Remarks:

    2 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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 Authors to J.G. Simmonds

    ALLAX B. PIFKO AND MARTIN A. GOLDBERG | AIAA | 1964