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)
Simmonds. Simmonds' "Spartan."
Aviation
Aviation ; 25 , n 9
1928
1 Fig.
Article (Journal)
English
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Simmonds. Simmonds' "Spartan."
Engineering Index Backfile | 1928
Simmonds. Simmonds' "spartan."
Engineering Index Backfile | 1928
Simmonds. Simmonds' "Spartan."
Engineering Index Backfile | 1928
Engineering Index Backfile | 1929
SIMMONDS FUEL INJECTION SYSTEM FOR GASOLINE ENGINES
SAE Technical Papers | 1955
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