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Fokker D.VIII

Pioneer and Early Aviation Aircraft

The Fokker D.VIII, first known as the Fokker E.V, was a German parasol-monoplane fighter designed by Reinhold Platz and built by Fokker-Flugzeugwerke. It was the last Fokker design to become operational with the German air service, entering service in the last months of World War I. Its prototype V.26 won an order at the second Adlershof fighter trials in May and June 1918, and all production aircraft used the 82 kW Oberursel Ur.II rotary engine. After several fatal accidents caused by wing failures the aircraft was grounded, modified and renamed D.VIII. Dubbed the Flying Razor by post-war pulp-fiction writers, it scored the last aerial victory of the war.

Facts
Year
1918 1
Engine Class
Piston 1
Power (kW)
82 1
Top Speed (km/h)
204 1
Mass (kg)
405 1
Maximum Mass (kg)
605 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Fokker D.VIII (Wikipedia)

Of Make

Source Fokker D.VIII (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Fokker D.VIII (Wikipedia)Lead
Quote, Lead
The Fokker E.V was a German parasol-monoplane fighter aircraft designed by Reinhold Platz and built by Fokker-Flugzeugwerke.

Originated In

Also in Geography Atlas: where this subject originated.

Source Fokker D.VIII (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
was a German parasol-monoplane fighter aircraft
Sources
1. Fokker D.VIII (Wikipedia)
  • Development and service
    In early 1918, Fokker produced several rotary-powered monoplane prototypes
  • Lead
    The Fokker E.V was a German parasol-monoplane fighter aircraft designed by Reinhold Platz and built by Fokker-Flugzeugwerke.
  • Specifications (D.VIII)
    Empty weight: 405 kg (893 lb)
  • Specifications (D.VIII), maximum mass
    Gross weight: 605 kg (1,334 lb)
  • Specifications (D.VIII), top speed
    Maximum speed: 204 km/h (127 mph, 110 kn)
  • Specifications (D.VIII), power
    Powerplant: 1 × Oberursel UR.II 9-cyl. air-cooled rotary piston engine, 82 kW (110 hp)
  • Specifications (D.VIII), engine
    Powerplant: 1 × Oberursel UR.II 9-cyl. air-cooled rotary piston engine, 82 kW (110 hp)
  • Lead, country of origin
    was a German parasol-monoplane fighter aircraft
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