The Gloster Gladiator



Gloster Aircraft Company.

Type: Single-seat fighter
Description  Bi-Plane

Wingspan  Span 32ft 3.in (9.85m)
Length 27ft Sin (8.38m);
Height 10 ft 4 in (3.17m).
Weight empty 3.4501b (1565kg)
Weight loaded 4,7501b (2155kg)
Power Plant : One 840hp Bristol Mercury IX or IXS nine-cylinder radial
 Armament Four 0.303in Browning's

Performance
Maximum speed :253mph
Initial Climb rate  2.300ft (700m) min
Ceiling : 33,000ft (10,060m)
Range : Range 440 miles
First Flight : (S.S.37) September 1934
Service Entry : March 1937
Users: Belgium, China. Egypt, Finland. Greece. Iraq. Ireland. Latvia, Lithuania. Norway. Portugal, South Africa, Sweden, UK (RAF. RN)


 
Development: Air Ministry Specification F.7/30 recognized that future fighters would have to be faster and better armed, but the delay in placing an order extended to a disgraceful
4 1/2 years, by which time war clouds were distantly gathering and the fabric-covered biplane was swiftly to be judged obsolete. Folland's S.S.37 was built as a very late entrant. long after the competition to F.7130 ought to have been settled. Though less radical than most contenders it was eventually judged best and. as the Gladiator, was at last ordered in July 1935. Features included neat single-bay wings, each of the four planes having small hydraulically depressed drag flaps; cantilever landing gear with Dowty internally sprung wheels; four guns; and. in the production aircraft. a sliding cockpit canopy. Most early production had the Watts wooden propeller, though performance was better with the three-blade metal Fairey- Reed type. The Mk II aircraft introduced desert filters. auto mixture control and electric starter from internal battery. The Sea Gladiator had full carrier equipment and a dinghy. Total production amounted to at least 767, including 480 for the RAF.


Squadrons that Flew the Gladiator during the Battle of Britain.
No 247 Squadron
No 804 Squadron
No 808 Squadron

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