| Featuring a fuselage virtually identical to that of the D.I,
the D.II was flown as a prototype in the summer of 1917,
this, the Aviatik 30.22, actually employing much of the
structure of the 30.21 (see D.I). The D.II was characterised
by a short-span cantilever lower wing, and a
series of 19 aircraft was built for frontline evaluation,
these being powered by either the 200hp (Series 39) or
225hp (Series 339) Austro-Daimler engine. A fourbladed
Jaray propeller was fitted, and armament consisted of the usual paired Schwarzlose 8mm guns. The
first three series aircraft were tested in November 1917,
and seven were evaluated at the front, but the decision
that O-UF Aviatik should licence-manufacture the
Fokker D.VII terminated any plans to build the D.II in
quantity. One D.II airframe was experimentally fitted
with a 200hp Hiero engine as the Aviatik 30.38, and
participated in the July 1918 D-Contest. With the 225hp
Austro-Daimler engine the D.II attained 220km/h.
 | A three-view drawing (1280 x 998) |
WEIGHTS |
Take-off weight | 810 kg | 1786 lb |
Empty weight | 587 kg | 1294 lb |
DIMENSIONS |
Wingspan | 7.50 m | 25 ft 7 in |
Length | 6.98 m | 23 ft 11 in |
PERFORMANCE |
Max. speed | 210 km/h | 130 mph |
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