Fokker E.II
The Fokker E.II was the second variant of the German Fokker Eindecker single-seat monoplane fighter aircraft of World War I. The E.II was essentially a Fokker E.I with the 75 kW (100 hp) Oberursel U.I 9-cylinder rotary engine, a close copy of the French Gnôme Monosoupape rotary of the same power output, in place of the E.I's 60 kW (80 hp) Oberursel U.0, but whereas the E.I was simply a M.5K with a 7.92 mm (.312 in) machine gun bolted to it, the E.II was designed with the weapon system integrated with its airframe.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Fokker
- First flight
- 1915-06-13
Specifications
- Cruise speed
- 76 kt
- Max speed
- 76 kt
- Max takeoff weight
- 1,102 lb
- Empty weight
- 750 lb
- Fuel capacity
- 23.8 US gal
- Powerplant
- Oberursel U.I 9-cyl. air-cooled rotary engine
- Engines
- 1
- Seats
- 1
- Length
- 23.6 ft
- Wingspan
- 31.8 ft
- Height
- 9.2 ft
- Number built
- 49
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.