| Flown as a prototype on 5 May 1923, the D XI single-seat
fighter was of sesquiplane configuration. Powered
by a 300hp Hispano-Suiza 8Fb eight-cylinder water-cooled
engine and carrying an armament of two synchronised
7.92mm LMG 08/15 machine guns, the D XI
had a fabric-covered steel-tube fuselage and plywood
covered wooden wings. One hundred and twenty-five
were ordered by the Soviet government, and a further
50 were ordered on behalf of Germany's Reichswehr by
the financier Hugo Stinnes for the clandestine German
air training centre, which, in 1924, was being established
at Lipetsk, north of Voronezh, in the Soviet
Union. In the event, the German order was cancelled
and, in 1925, these 50 D XIs were sold to Romania. Two
others were supplied to Switzerland in 1925 for evaluation
by that country's Fliegertruppe, and earlier, at
the beginning of 1924, three had been delivered to
McCook Field for evaluation by the US Army Air Service as PW-7s. The three D XIs supplied to the USAAS were
non-standard in having the 440hp V-1150 (Curtiss D-12)
water-cooled engine. The first of these had standard
plywood-covered wings with V-type interplane struts,
and the second and third had fabric wing skinning and
N-type strutting.
 | A three-view drawing (1278 x 894) |
WEIGHTS |
Take-off weight | 1250 kg | 2756 lb |
Empty weight | 865 kg | 1907 lb |
DIMENSIONS |
Wingspan | 11.67 m | 38 ft 3 in |
Length | 7.50 m | 25 ft 7 in |
Height | 3.20 m | 11 ft 6 in |
Wing area | 21.80 m2 | 234.65 sq ft |
PERFORMANCE |
Max. speed | 225 km/h | 140 mph |
Range | 440 km | 273 miles |
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