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UFAG D.I

The Ufag D.I was a high-wing monoplane with monocoque fuselage, powered by a Le Rhône(St) engine. Although there is no direct evidence, it is highly likely that the D.I under construction was the Ufag 60.02.[1]

Variants

D.I
Service designation for proposed production aircraft
Ufag 60.02
probable designation for the first D.I prototype under construction at the time of the armistice.

Specifications (60.03 / D.I)

Data from Austro-Hungarian Army Aircraft of World War One[1]

General characteristics

  • Crew: 1
  • Wingspan: 8.5 m (27 ft 11 in)
  • Wing area: 15.6 m2 (168 sq ft)
  • Empty weight: 380 kg (838 lb)
  • Gross weight: 630 kg (1,389 lb)
  • Powerplant: 1 × Le Rhône(St) 9-cylinder air-cooled rotary piston engine, 110 kW (150 hp)

Performance

Citations

  1. ^ a b Grosz, Peter M. (2002). Austro-Hungarian Army Aircraft of World War One. Colorado: Flying Machine Press. p. 265.

Bibliography

  • Green, William & Swanborough, Gordon (2001) [1994]. The Complete Book of Fighters: An Illustrated Encyclopedia of Every Fighter Built and Flown (Revised and Updated ed.). London: Salamander Books. ISBN 1-84065-269-1.
  • Grosz, Peter Michael; Haddow, George & Schiemer, Peter (1993). Austro-Hungarian Army Aircraft of World War One. Mountain View, California: Flying Machines Press. ISBN 0-9637110-0-8.