|First flight||28 March 1925|
The Fokker D.XIV was a fighter aircraft developed in the Netherlands in the mid-1920s but which was only produced as a single prototype. It was a low-wing, cantilever monoplane with fixed tailskid undercarriage, the basic concept of which was derived from the Fokker V.25 that had been developed during World War I. The pilot sat in an open cockpit aft of the wing's trailing edge. Flight testing revealed excellent performance, but development was ceased when the prototype crashed, killing the test pilot.
Specifications[edit | edit source]
- Crew: One pilot
- Length: 7.90 m (25 ft 11 in)
- Wingspan: 10.76 m (35 ft 4 in)
- Height: 3.25 m (10 ft 8 in)
- Empty weight: 950 kg (2,090 lb)
- Gross weight: 1,350 kg (2,980 lb)
- Powerplant: 1 × Hispano-Suiza 12Hb, 440 kW (590 hp)
- Maximum speed: 274 km/h (170 mph)
- Rate of climb: 7.1 m/s (1,400 ft/min)
References[edit | edit source]
|Wikimedia Commons has media related to Fokker aircraft.|
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 405.
- "Two New Fokker Military Aeroplanes". 30 April 1925. pp. 261. http://www.flightglobal.com/PDFArchive/View/1925/1925%20-%200261.html. Retrieved 2008-03-26.
- Уголок неба
|This page uses Creative Commons Licensed content from Wikipedia (view authors).|