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During 1939, Martin-Baker Aircraft designed a new
fighter around which was drawn up Specification
F.18/39. As with its predecessor the precepts of structural
simplicity and sturdiness dominated the design.
The fuselage still made use of a patented system of
steel tubes, but the skin was stressed light alloy and
the wing had a more conventional torsion box structure.,
Three prototypes were ordered and, designated
M.B.3, the first of these was flown on 31 August 1942
with a 2020hp Napier Sabre II 24-cylinder horizontal-H
type engine. Armament comprised six 20mm cannon.
Only limited handling and performance data had been
obtained when, on 12 September 1942, the M.B.3 was
destroyed in an accident. Extensive redesign was introduced
prior to the completion of the second prototype,
which emerged as the M.B.5.
 | A three-view drawing (1280 x 930) |
| WEIGHTS |
| Take-off weight | 5215 kg | 11497 lb |
| DIMENSIONS |
| Wingspan | 10.67 m | 35 ft 0 in |
| Length | 10.77 m | 35 ft 4 in |
| Height | 4.74 m | 15 ft 7 in |
| Wing area | 24.40 m2 | 262.64 sq ft |
| PERFORMANCE |
| Max. speed | 668 km/h | 415 mph |
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