Dewoitine D 12
1924
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Dewoitine D 12

Evolved in parallel with the D 9 as a contender in the 1923 C1 programme, in which it was eventually to take third place after the Nieuport-Delage 42 and the Gourdou- Leseurre 32, the D 12 differed essentially in engine type. Possessing a basically similar fuselage to that of the D 1, the D 12 was powered by a 450hp Lorraine- Dietrich 12EW 12-cylinder W-type water-cooled engine. First flown, like the D 9, in June 1924, the D 12 had an armament of two 7.7mm Vickers guns, and, in September, was fitted with a higher compression ratio 12Eb engine and a pair of 7.5mm Darne modele 19 guns on the wing centre section. The paired Lamblin radiators on the undercarriage legs gave place to a frontal radiator and a wing similar to that finally adopted on the D 9 was fitted. On 5 February 1926, the D 12 was written off in an accident at Cazaux. A second prototype had meanwhile entered flight test, having flown at the end of 1925, this having a W-type Hispano-Suiza 12Gb engine, but further development was discontinued.


Specification 
 WEIGHTS
    Take-off weight1636 kg3607 lb
    Empty weight1070 kg2359 lb
 DIMENSIONS
    Wingspan12.80 m41 ft 12 in
    Length7.60 m24 ft 11 in
    Height3.00 m9 ft 10 in
    Wing area25.00 m2269.10 sq ft
 PERFORMANCE
    Max. speed239 km/h149 mph

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