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Late in 1944, Gloster began construction of an all-metal
single-seat fighter designed around the RB.41 centrifugal-
flow turbojet being developed by Rolls-Royce and
to emerge as the Nene. To the requirements of Specification
E.1/44, the first prototype was completed in July 1947, but suffered irreparable damage when the
vehicle transporting it to the A&AEE was involved in
an accident. A second prototype was completed and
flown on 9 March 1948, this being powered by a
2268kg Nene 2 turbojet and having provision
for four 20mm Hispano cannon. After initial
flight testing the tail assembly was redesigned to improve
handling. A third prototype was flown in 1949,
and a fourth was nearing completion when it was
decided that the single-engined fighter lacked the development
potential of the twin-engined Meteor,
further work being discontinued.
 | A three-view drawing (1670 x 1203) |
| WEIGHTS |
| Take-off weight | 5203 kg | 11471 lb |
| Empty weight | 3747 kg | 8261 lb |
| DIMENSIONS |
| Wingspan | 10.97 m | 35 ft 12 in |
| Length | 11.58 m | 37 ft 12 in |
| Height | 3.55 m | 11 ft 8 in |
| Wing area | 23.60 m2 | 254.03 sq ft |
| PERFORMANCE |
| Max. speed | 998 km/h | 620 mph |
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