The Fokker V.17 and its derivatives were a series of experimental monoplane Fighter aircraft produced by the Dutch aircraft company Fokker in the 1910s.
5-484: (Redirected from V-25 ) V25 may refer to: Fokker V.25 , a Dutch experimental fighter aircraft NEC V25 , a microcontroller V25 -class torpedo boat , of the Imperial German Navy SMS ; V25 , the lead boat of the class [REDACTED] Topics referred to by the same term This disambiguation page lists articles associated with
10-504: The German Army and rejected due to poor forward visibility (presumably on landing). The V.23 was powered by a 119 kW (160 hp) Mercedes III engine, was 5.8 m (19 ft) long, had a wingspan of 8.73 m (28.64 ft), a height of 2.65 m (8.69 ft). The wing area was 11.12 m² (119.69 ft²), the empty weight was 673 kg (1,484 lb), maximum weight 853 kg (1,881 lb). The maximum speed of
15-446: The V.23 was 200 km/h (124 mph). Armament was two 7.92 mm (.312 in) machine guns. V.25 was plywood-covered, with a low cantilever wing. It powered by an Oberursel Ur. II of 82 kW (110 hp). The aircraft was underpowered. V.25 was 5.93 m (18.46 ft) long, had a wing span of 8.73 m (28.64 ft) and was 2.63 m (8.63 ft) high. Its wing area was 11.12 m² (119.69 ft²), empty weight
20-505: The same title formed as a letter–number combination. If an internal link led you here, you may wish to change the link to point directly to the intended article. Retrieved from " https://en.wikipedia.org/w/index.php?title=V25&oldid=1160389994 " Category : Letter–number combination disambiguation pages Hidden categories: Short description is different from Wikidata All article disambiguation pages All disambiguation pages Fokker V.25 V.17,
25-403: Was a shoulder cantilever -winged monoplane with plywood covering. 82 kW (110 hp) Oberursel engine. V.20, was a cantilever mid-winged fighter with plywood covering and was powered by a 119 kW (160 hp) Mercedes D IIIa engine. It was similar to the V.17. V.21 was much like the V.20 except the wings were tapered. V.23 was related to the V.20 and V.21. It was evaluated by
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