SHORT S.31

SHORT S.31 - After receiving orders for two prototypes and 100 production aircraft to the S.29 design which became the Short Stirling, Shorts built in 1938 a '/2-scale prototype at its own expense. Powered by four 90 hp Pobjoy Niagara III engines, this Short S.31 was mostly of wooden construction apart from a semi-monocoque fuselage, and seated two in tandem. In overall silver finish and marked M4, the Short S.31 flew on September 19, 1938, at Rochester. It later acquired a lengthened u/c (as adopted meanwhile on the Short S.29 to give greater effective wing incidence during take-off and landing); then in January 1939 it was fitted with 115 hp Niagara IVs and in March with a larger tailplane. In 1940, now in green/brown camouflage with yellow undersides, the Short S.31 was fitted with Va-scale mock-ups of the Boulton Paul Type O ventral and Type H dorsal twin-cannon turrets proposed for a version of the Stirling II, and was tested in the RAE 24 ft (7.3 m) wind tunnel. Further flights were made from March 13, 1942, onwards (with a shortened u/c), and the Short S.31 was scrapped after a takeoff accident at Stradishall in February 1944. Max speed, 180 mph (290 kmlh). Gross weight, 5,700 Ib (2,586 kg). Span, 49 ft 6'h in (15.09 m). Length, 43 ft 7'h in (13.31 m).