Chris's Gloster Gladius build in Current and Finished Projects:
http://www.whatifmodelers.com/index.php/topic,21222.0.htmlhas prompted me to post some info on the aircraft.
Part 1
The story begins in 1933 with specification F.5/33 for a two-seat fighter with turret armament, basically a replacement for the Hawker Turret Demon.
Gloster's design to F.5/33 was twin-engined with a four-gun power-operated turret and nose-mounted MGs to be powered by two 625 hp Bristol Aquila sleeve-valve engines.
No prototypes were built to F.5/33, the two other design studies to the specification were the Armstong-Whitworth AW.34 and the Bristol 140.
In 1935 the work on F.5/33 formed the basis of design work to meet specification F.34/35. This resulted in a proposal for a twin-engined two-seat-fighter, mounting a four-gun power-operated turret and with a fixed armament in the nose. RAF serial number K8625 was allocated for the prototype but it was abandoned when the Boulton Paul Defiant to spec. F.9/35 was ordered.
(See first image)
Specification F.9/37 was issued on 15th September 1937, calling for a twin-engined fighter capable of at least 300mph. The G.39 was designed to the specification. Two cockpits housed the pilot and an observer-gunner. Armament was a pair of 20mm cannon in the nose and a retractable turret with four .303 MG for the observer-gunner. Engines specified were R-R Kestrel or Bristol Taurus.
(See second image, the James and Buttler books state that the photo is of a model of the F.34/35, I feel that it is actually of the original G.39 - F.9/37 configuration)
In late 1938 the decision was taken to eliminate the amidships cockpit/turret and the G.39 was thus completed as a fixed armament single-seater.
Two forward firing 20mm Hispano cannon were placed beneath the pilot just forward of the rear spar and wee inclined at a 'no-allowance' angle of 12 degree to the line of flight. A proposal was made in November of 1938 to replace the turret with a battery of 20mm cannon fixed a the same angle in the upper fuselage behind the pilot to fire forward over the cockpit. (As to the number of cannon in this battery; Buttler states three, James and Mason give the quantity as four). The idea was accepted but photographic evidence suggests that the rear cannon were never fitted to either prototype, both aircraft did carry their nose armament.
L7779 was completed with two 1,050 hp Bristol Taurus T-S(a) and achieved a level speed of 360 mph.
After being damaged in a landing accident on 27 July 1939 the aircraft was re-engined with 900 hp Bristol Taurus T-S(a) IIIs.
The aircraft did not fly again until April 1940, top speed was reduced to 332mph and other performance suffered equally.
Due to engine and airframe serviceability problems trials were not completed until July 1940.
L8002 was completed with the 885hp Rolls-Royce Peregrine, top speed was further reduced to 330 mph.
(See third image for L8002)
Jon
Sources:
"Gloster Aircraft since 1917", Derek N. James, 2nd ed, 1987, Putnam
"The British Fighter since 1912", Francis K. Mason, 1992, Putnam/Naval Institute Press
"BSP: Fighters & Bombers 1935-1950", Tony Buttler, 2004, Midland