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Fokker D.I
D.I | |
---|---|
Type | Fighter aircraft |
Manufacturer | Fokker |
Designed by | Martin Kreutzer |
Introduced | 1916 |
Produced | July 1916 |
Number built | 114 |
Developed from | Fokker D.II |
Variants | D.III and D.IV. |
The Fokker D.I (company model M18) was a development of the D.II fighter. Confusing the matter further, both aircraft arrived at the Front in German service at similar times, in July-August 1916. The main designer was Martin Kreutzer.
Similar to the D.II, the D.I was an unstaggered single-bay equal-span biplane. The upper fuselage was parallel with the upper wing. Unlike the D.II, the D.I was fitted with the 100 hp Mercedes D.I six cylinder watercooled engine.
Control was achieved using wing-warping. The wings were also tested in twin bay form. To improve visibility, the center section was cut into and the wings were slightly staggered.
These improvements were retained, and the airplane was ordered into production with a 120 hp Mercedes D.II inline engine and a single synchronized LMG 08/15 machine gun.
Deliveries began in July 1916. 90 were delivered to the German Fliegertruppen, and 16 to the Austro-Hungarian Luftfahrttruppen (as the B III). Eight were license produced by the Magyar Általános Gépgyár in Hungary.
One Austro-Hungarian B III was experimentally fitted with a 160 hp Mercedes D.III engine. Another had ailerons instead of wing warping, and still another had long span, swept back wings.
Compared with aircraft in service at that time, such as the Albatros D.II and the Nieuport 11, this Fokker's design and performance were decidedly unimpressive, and further production did not take place.
The D.I was the basis for the D.III and D.IV.
Operators
- Template:Country data Austria-Hungary
- Austro-Hungarian Imperial and Royal Aviation Troops
- Template:Country data German Empire
- Luftstreitkräfte
Specifications (D.I)
General characteristics
- Crew: One, pilot
- Length: 6.30 m (20 ft 8 in)
- Wingspan: 9.05 m (29 ft 8 in)
- Height: 2.55 m (8 ft 4 in)
- Wing area: 20.00 m² (215.3 ft²)
- Empty weight: 463 kg (1,020 lb)
- Loaded weight: 820 kg (1,809 lb)
- Powerplant: 1× Mercedes D.II 6-cylinder water-cooled inline engine, 90 kW (120 hp)
Performance
- Maximum speed: 150 km/h (81 knots, 93 mph)
- Rate of climb: 3.33 m/s (656 ft/min)
- Endurance: 1.5 hours
Armament
See also
Comparable aircraft
Albatros D.I -
Nieuport 11
Designation sequence
D.II -
D.I -
D.III -
D.IV -
D.V -
Dr.I -
D.VI -
D.VII -
D.VIII -
D.IX -
Related lists
Lists relating to aviation | |
---|---|
General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
Military | Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft |
Notable incidents and accidents | Military aviation · Airliners · General aviation · Famous aviation-related deaths |
Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
Lists relating to aviation | |
---|---|
General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
Military | Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft |
Notable incidents and accidents | Military aviation · Airliners · General aviation · Famous aviation-related deaths |
Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
Template:Idflieg fighter designations
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Fokker D.I". |