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
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
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)LeadQuote, 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 originQuote, 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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