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Fokker E.IV

Pioneer and Early Aviation Aircraft

The Fokker E.IV was the final variant of the Eindecker fighter operated by Germany in World War I. Given the Fokker designation M.15, it was essentially a lengthened E.III powered by the 119 kW Oberursel U.III two-row, 14-cylinder rotary engine, a copy of the Gnome Double Lambda, which was meant to let it carry two or three 7.92 mm machine guns. The heavier engine made the aircraft much less manoeuvrable than the E.III, and the engine lost power after only a few hours of use. Only 49 E.IVs were built out of a total Eindecker production run of 416, and over half entered service in June 1916, when they were already obsolete. Production E.IVs standardised the fitting of twin synchronized machine guns.

Facts
Year
1915 1
Engine Class
Piston 1
Power (kW)
119 1
Units Built
49 1
Top Speed (km/h)
170 1
Mass (kg)
466 1
Maximum Mass (kg)
724 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Fokker E.IV (Wikipedia)

Of Make

Source Fokker E.IV (Wikipedia)
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Manufactured By

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Source Fokker E.IV (Wikipedia)Lead
Quote, Lead
The Fokker E.IV was the final variant of the Eindecker fighter aircraft that was operated by Germany during World War I.

Originated In

Also in Geography Atlas: where this subject originated.

Source Fokker E.IV (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
accepted for testing by the German Inspektion der Fliegertruppen
Sources
1. Fokker E.IV (Wikipedia)
  • Development and service
    The prototype E.IV was accepted for testing by the German Inspektion der Fliegertruppen in September 1915.
  • Lead
    The Fokker E.IV was the final variant of the Eindecker fighter aircraft that was operated by Germany during World War I.
  • Operational history
    Only 49 E.IVs were built out of the total Eindecker production run of 416 aircraft.
  • Specifications (E.IV)
    Empty weight: 466 kg (1,027 lb)
  • Specifications (E.IV), maximum mass
    Max takeoff weight: 724 kg (1,596 lb)
  • Specifications (E.IV), top speed
    Maximum speed: 170 km/h (110 mph, 92 kn)
  • Specifications (E.IV), power
    Powerplant: 1 × Oberursel U.III 14-cyl. two-row air-cooled rotary piston engine, 119 kW (160 hp)
  • Specifications (E.IV), engine
    Powerplant: 1 × Oberursel U.III 14-cyl. two-row air-cooled rotary piston engine, 119 kW (160 hp)
  • Lead, country of origin
    accepted for testing by the German Inspektion der Fliegertruppen
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