Even before the Stirling went into production, Short had improved on
the initial design with the S.34 in an effort to meet
specification B.1/39. It would have been powered by four Bristol Hercules 17 SM
engines, optimised for high-altitude flight. The new design featured longer span
wings and a revised fuselage able to carry dorsal and ventral power-operated
turrets each fitted with four 20 mm Hispano cannon; despite the obvious gains in
performance and capability, the Air Ministry was not interested.
In 1941,
Short proposed an improved version of the Stirling, optimistically called "The
Super Stirling" in the company's annals. This Stirling would feature a wing span
of 135 ft 9 in (41.38 m) and four Bristol Centaurus radials and a maximum
takeoff weight of 104,000 lb (47,174 kg). The performance estimates included 300
mph (483 km/h) speed and a 4,000 mile (6,437 km) range with a weapons load of
10,000 lb (4,536 kg) over 2,300 miles or 23,500 lb over 1,000 miles. Defensive
armament was 10 0.5 inch machine guns in three turrets. It was initially
accepted for under Specification B.8/41 (written to cover it) and two prototypes
were ordered but the C-in-C of Bomber Command Arthur Harris felt that, while it
would be a better aircraft, actual production would be slower and that effort
would be better spent on giving the Stirling improved Hercules engines for a
higher ceiling. Shorts were told in May 1942 that the Air Ministry would not be
continuing the project and in August Shorts decided to terminate work.