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Data from Vickers Aircraft since 1908 General characteristics Crew: two Length: 36 ft 5 in (11.10 m) Wingspan: 47 ft 6 in (14.48 m) Wing area: 290 sq ft (27 m 2) Empty weight: 1,000 lb (454 kg) Powerplant: 1 × R.E.P five-cylinder air-cooled fan-type engine, 60 hp (45 kW) Performance Maximum speed: 56 mph (90 km/h, 49 kn) Notes ^ Flight 15 April 1911, p.336. ^ Andrews and Morgan 1988, p. 1 ...
The Vickers Wellesley was a medium bomber that was designed and produced by the British ... The private venture monoplane, ... Maximum speed: 228 mph (367 ...
The Vickers Type 559 was a supersonic interceptor aircraft design by the British aircraft company Vickers-Armstrongs and was their submission for Operational Requirement F.155 in 1955. It was not accepted for further consideration; the most valued submissions being from Armstrong Whitworth and Fairey , however the F.155 requirement was dropped ...
The REP Type N was a military reconnaissance monoplane produced in France in 1914. [1] ... Maximum speed: 116 km/h (73 mph, 63 kn) See also
It was followed by a further 19 aircraft built wholly by Canadian Vickers, production continuing until October 1940. [8] The Northrop Delta was the first completely all-metal, stressed-skin aircraft built in Canada, however it was closely preceded by the Fairchild Super 71 , whose stressed skin construction was limited to the fuselage and not ...
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Developed from the earlier Wib.3 the Wibault 7 was a C.I category single-seat high-wing braced parasol monoplane fighter powered by a 480 hp (360 kW) Gnome-Rhone 9Ad radial engine. The main difference from earlier aircraft was the use of an all-metal construction system which was patented by Wibault.
The specification required a range of 920 mi (1,480 km) at a speed of 115 mph (185 km/h), with a bomb load of 1,500 lb (680 kg). [2] To meet this requirement, Fairey designed a low-winged cantilever monoplane with a fixed tailwheel undercarriage. The fuselage had a steel tube structure with fabric covering with a pilot, a radio operator ...