Arado SSD I


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Arado SSD I

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.

Arado SSD IA three-view drawing (1637 x 1080)

  Take-off weight2030 kg4475 lb
  Empty weight1627 kg3587 lb
  Wingspan10.00 m33 ft 10 in
  Length8.50 m28 ft 11 in
  Wing area31.00 m2333.68 sq ft
  Max. speed280 km/h174 mph

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