Dornier Do 212
| Dornier Do 212 | |
|---|---|
| Type: | single-engine amphibious aircraft |
| Design country: | |
| Manufacturer: | |
| 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
- ↑ No. 4219. Dornier Do 212 V1 (HB-GOG). In: www.1000aircraftphotos.com. May 22, 2005, accessed June 26, 2020 .
- ↑ a b c d Dornier Do 212. In: http://histaviation.com . Retrieved June 26, 2020 (English).