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Dornier Do 212

From Wikipedia, the free encyclopedia
Flying boat
Do 212
General information
TypeFlying boat
National originSwitzerland/Germany
ManufacturerDornier Flugzeugwerke
Number built1
History
First flightAugust 1942

TheDornier Do 212 was a four-seat experimentalamphibianflying boat built by theSwiss subsidiary ofDornier, inAltenrhein onLake Constance. Design was initiated in 1938 by theGerman and Swiss branches, the latter being responsible for the actual construction of theprototype.

The Do 212 was an all-metalcantilevermonoplane with fixed wingtip floats and a 343 kW (460 hp)Hirth HM 512-B-0 12-cylinder air-cooled engine which, mounted aft of thecabin, was buried in thefuselage and drove a four-blade airscrew aft of the tail by means of a shaft which could be tilted upward 12° to provide water clearance.

Initial water taxiing trials resulted in the enlarging of the wingtip floats. On 3 August 1942, a few attempts to take off from water were made, but these failed. ADo 24 was used to tow the Do 212 and it finally flew; however, instability forced the pilot to ditch just after takeoff. Further trials ended the same way. Difficulties were also experienced with the extension shaft, and the cooling of the engine presented a problem. Consequently, no further testing was undertaken, and the prototype was scrapped in 1943.

Specifications (Do 212)

[edit]

Data from[1]

General characteristics

  • Crew: one
  • Capacity: three
  • Length: 10.15 m (33 ft 4 in)
  • Wingspan: 10.3 m (33 ft 10 in)
  • Height: 4.4 m (14 ft 5 in)
  • Wing area: 23.1 m2 (249 sq ft)
  • Empty weight: 1,850 kg (4,079 lb)
  • Gross weight: 2,370 kg (5,225 lb)
  • Fuel capacity: fuel - 250 L (55 imp gal) , oil - 30 L (7 imp gal)
Stabiliser Span
6.52 m (21 ft) with 8° 30' dihedral
  • Powerplant: 1 ×Hirth HM 512B-0 inverted 60° V-12 air-cooled piston engine, 330.9 kW (443.8 hp)
  • Propellers: 4-bladedEscher-Wyss, 2.40 m (7 ft 10 in) diameter driven via a 2.9 m (10 ft) extension shaft raised 12° for take-off and landing.

Performance

  • Maximum speed: 293 km/h (182 mph, 158 kn) (estimated)
  • Cruise speed: 240 km/h (150 mph, 130 kn)
  • Range: 650 km (400 mi, 350 nmi) (estimated)
  • Service ceiling: 5,700 m (18,700 ft) (estimated)
  • Rate of climb: 0.476 m/s (93.7 ft/min) (estimated)
  • Time to altitude:
    • 1,000 m (3,281 ft) in 35 minutes (estimated)
    • 3,000 m (9,843 ft) in 105 minutes (estimated)

References

[edit]
  1. ^"Dornier_Do_212". Germany. Retrieved25 February 2012.

External links

[edit]
Dornier and Zeppelin-Lindau aircraft
Zeppelin-Lindau
1914-1919
Dornier designations
1919-1933
RLM designations
1933-1945
Dornier designations
post-1945
1 to 100
101 to 200
201 to 300
301 to 349
Post-349 (non-sequential)
  • 1 Not assigned
  • 2 Unofficial/proposed
  • 3 Assigned, but not used before RLM was dissolved
  • 4 Assigned to captured aircraft
  • 5 Unconfirmed
  • 6 Propaganda/cover designation
  • 7 Assigned to multiple types

Note: Official RLM designations had the prefix "8-", but this was usually dropped and replaced with the manufacturer's prefix.

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