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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 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 ...
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Hanriot 1912 Monoplane: Hanriot (England) Limited £100 for completing trial 2 Hanriot 1912 Monoplane Hanriot (England) Limited £100 for completing trial 3 Vickers Monoplane No. 6: Vickers Limited Completed trial 4 Blériot XI-2: Louis Bleriot: Tandem seating, £100 for completing trial, purchased by the Royal Flying Corps after trial 5 ...
The R.E.P. 1 in 1907. The REP 1 was a single-seat tractor configuration monoplane powered by a 22 kW (30 hp) seven-cylinder two-row semi-radial engine [1] driving a four-bladed propeller with aluminium blades rivetted to steel tubes.
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The Type 151 Jockey was a compact and rather angular, low cantilever wing monoplane, built using the Wibault-Vickers corrugated skinned all-metal method as used on the Vireo. The unstressed skin was riveted onto a largely duralumin structure, a few steel tubes forming highly stressed members.
In January 1915, the two units merged and were re-equipped with Caudron G.3s, but continued to operate the REP Type N at least as late as March. [ 2 ] The Type N also formed the backbone of the Ottoman Air Service in 1912, and these machines were used operationally during the First and Second Balkan War in 1912–13. [ 2 ]