| Built in 1930 as a catapultable single-seat float fighter,
the SSD I possessed no commonality with other Arado
fighters of the period. A single-bay equi-span biplane
with plywood-covered wooden wings with N-type
interplane struts, and, unlike preceding fighter aircraft
from the Warnemünde-based company, ailerons in
both upper and lower wings, the SSD I was powered by
a 640hp BMW VI 6.3 12-cylinder Vee-type watercooled
engine. The upper wing was gulled into the top
decking of the welded steel-tube fuselage ahead of the
cockpit and the lower wing was suspended below the
fuselage, the gap being occupied by the tunnel-type
radiator. Initial water trials were conducted at Travemünde with a central main float and twin outrigger stabilising
floats. The SSD I was subsequently fitted with a
somewhat rudimentary wheel undercarriage to permit
trials at Lipezk, the clandestine German flying school in
the Soviet Union, where the armament of twin 7.9mm
guns was fitted. The Heinkel HD 38 was selected in
preference to the SSD I, the sole prototype of which was
assigned in April 1932 to the Luftdienst GmbH, and, a
year later, to the Deutsche Verkehrsfliegerschule
(DVS), the German commercial pilots' school. The following
data relate to the SSD I with wheel undercarriage.
 | A three-view drawing (1637 x 1080) |
WEIGHTS |
Take-off weight | 2030 kg | 4475 lb |
Empty weight | 1627 kg | 3587 lb |
DIMENSIONS |
Wingspan | 10.00 m | 33 ft 10 in |
Length | 8.50 m | 28 ft 11 in |
Wing area | 31.00 m2 | 333.68 sq ft |
PERFORMANCE |
Max. speed | 280 km/h | 174 mph |
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