Last update: 05 May 2009 Send to a friend PrintPrint

Dornier Delphin I

Delphin I was a single-engine all-metal high-wing monoplane. The two-step hull with its blunt bow was divided into several bulkheads and equipped with the Dornier sponsons. The all-metal wing consisted of two halves, each mounted to the lateral wall of the hull and braced with the sponsons by means of two struts. The power plant consisted of a BMW IIIa engine with a face-type radiator between the two-blade wooden propeller and the engine. The open flight deck equipped with a cover for test purposes, was located immediately aft of the engine. The cabin for 4-5 passengers and a baggage hold were located in the hull. The aircraft had a standard cross-shaped empennage.

First flight took place on November 24, 1920. During the test, the blunt bow of the hull was very unfavorable during the take-off phase. Therefore, the bow was extended. Four aircraft were built, two of them in the new Marina di Pisa/Italy plant. One Delphin I was taken over for testing of all-metal aircraft construction by the U.S. Navy. One Delphin I was delivered to the Japanese licensee, Kawasaki Dockyard Co. of Kobe.

Technical data

Dornier Delphin I

Power Plant BMW IIa with 136 kW

Performance

Top speed 125 km/h
Service ceiling 4,000 m

Weight

Empty weight 1,600 kg
Maximum take-off weight 2,200 kg

Dimensions

Length 11.5 m
Height 3.1 m
Wing span 17.1 m
Wing area 51,3 qm
Crew 1 person
Passengers 4-5 persons

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