Dornier Do 212

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Dornier Do 212
f2
Type: single-engine amphibious aircraft
Design country:

German Reich NSGerman Reich (Nazi era) German Empire / SwitzerlandSwitzerlandSwitzerland 

Manufacturer:

Dornier

First flight:

August 3, 1942

Number of pieces:

1 prototype

The Dornier Do 212 was a single-engine, four-seat amphibious aircraft produced by the Dornier-Werke .

The development was initiated in 1938 by Dornier Friedrichshafen and a prototype was constructed in the Dornierwerk Altenrhein from 1941 onwards. The aircraft was of an air-cooled 450-PS twelve-cylinder - V-engine Hirth HM 512B-0 with four-leaf pusher propeller driven, the m on a 2.9 jib over the stern with double tail out continuously for takeoff and landing by 12 ° to the top was. The cantilevered all-metal shoulder- wing wing had rigid support floats on the edge arches and a retractable nose wheel.

After completion of the HB-GOG prototype in 1942 and "roll tests" on the water, the support floats were enlarged. At the end of July 1942 the aircraft was ready for a flight test. On August 3, 1942, Egon Fath made a few unsuccessful attempts to launch himself out of the water. The first flight was only in towing a Do 24 . After later self-launch attempts also failed, the aircraft flew very unstably and problems with the long-distance shaft and engine cooling occurred, the project was abandoned and the prototype was scrapped in 1943.

Technical specifications

Parameter Data
crew 1
Passengers 3
length 10.15 m
span 10.30 m
height 4.40 m
Wing area 23.1 m²
(14.8 m² wing + 8.3 m² tailplane)
Wing extension 4.6
Empty mass 1850 kg
Takeoff mass 2370 kg
Cruising speed 240 km / h (projected)
Top speed 293 km / h (projected)
Service ceiling 5700 m (projected)
Range 650 km (projected)
Engines a Hirth HM 512B-0 , 450 PS (approx. 330 kW)
propeller an Escher-Wyss , four-leaved, 2.4 m in diameter

See also

Individual evidence

  1. No. 4219. Dornier Do 212 V1 (HB-GOG). In: www.1000aircraftphotos.com. May 22, 2005, accessed June 26, 2020 .
  2. a b c d Dornier Do 212. In: http://histaviation.com . Retrieved June 26, 2020 (English).