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Britten-Norman (BN) is a privately owned British aircraft manufacturer and aviation services provider. The company is the sole independent commercial aircraft producer in the United Kingdom. Britten-Norman has so far manufactured and sold its aircraft to customers in more than 120 countries.
Partners include Britten-Norman, Rolls-Royce plc for the power management system, Denis Ferranti for the electric motors, Delta Motorsport for the battery pack, and Warwick Manufacturing Group for battery testing. It targets a 60 min endurance plus 30 min reserves and with energy five times cheaper than Avgas and reduced maintenance, the ...
Britten-Norman Nymph [39] Britten Norman Islander; Britten-Norman Trislander; Fairey-Britten-Norman Mainlander [40] The aircraft was designed to carry 100 passengers or ten tonnes of freight or vehicles over 250 miles (400 km) at 200 kn (370 km/h; 230 mph). At the maximum take-off weight of 62,500 lb (28,300 kg) and sea level, ISA plus 20 °C ...
In 1951 Peter Gatrell, John Britten & Desmond Norman built and flew an ultra-light monoplane, their first aircraft, which made its first flight at Bembridge, Isle of Wight, on 16 May 1951. This machine crashed on an early flight, when the petrol supply to the 40 hp Aeronca-J.A.P. J-99 twin cylinder air-cooled engine faded out. [ 2 ]
In December 2006, aerospace publication Flight International observed that: "The only civil aircraft that remains in production in the UK is the tiny Britten-Norman Islander". [ 20 ] In early 2008, B-N was studying a version powered by 350 hp (260 kW) aircraft diesel engines with SMA Engines , already offering the 230 hp (170 kW) SMA SR305-230 ...
Aircraft engineer John Britten, who had been instrumental in founding Britten-Norman, left the company in February 1976. [2] After that, he began development of an economical four-place light twin aircraft, the Sheriff. It was a low-wing cantilever monoplane with twin tails and a tractor engine in a nacelle on each wing.
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Data from Jane's All the World's Aircraft 1988-1989 General characteristics Crew: 2 Length: 8.33 m (27 ft 4 in) Wingspan: 7.92 m (26 ft 0 in) Height: 3.25 m (10 ft 8 in) Wing area: 11.89 m 2 (128.0 sq ft) Aspect ratio: 5.28:1 Airfoil: NACA 23012 Empty weight: 1,117 kg (2,463 lb) Max takeoff weight: 1,633 kg (3,600 lb) Fuel capacity: 405 L (89 imp gal; 107 US gal) internal fuel Powerplant: 1 × ...