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H.7/42 OR.117 Torpedo bomber – Beaufighter replacement Bristol Brigand: R.8/42 OR.118 Long-range patrol/reconnaissance flying boat – Sunderland with Hercules engines Short Sunderland IV/Seaford: Q.9/42 OR.119 Twin engine target tug – planned production of Monitor later cancelled – see also Q.1/46 'Miles Monitor TT Mk.1: 10/42
Download as PDF; Printable version; ... ABC 170 hp V-12 [2] [4] ABC 225 hp V-16 ... Merged with Armstrong Siddeley in 1958 to form Bristol Siddeley. Sources: Piston ...
The Armstrong Siddeley Viper is a British turbojet engine developed and produced by Armstrong Siddeley and then by its successor companies Bristol Siddeley and Rolls-Royce Limited. It entered service in 1953 and remained in use with the Royal Air Force , powering its Dominie T1 navigation training aircraft until January 2011.
The Armstrong Siddeley Sapphire is a British turbojet engine that was produced by Armstrong Siddeley in the 1950s. It was the ultimate development of work that had started as the Metrovick F.2 in 1940, evolving into an advanced axial flow design with an annular combustion chamber that developed over 11,000 lbf (49 kN).
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1903: Charlie Taylor built an inline engine, mostly of aluminum, for the Wright Flyer (12 horsepower). 1903: Manly-Balzer engine sets standards for later radial engines. [3] 1906: Léon Levavasseur produces a successful water-cooled V8 engine for aircraft use. 1908: René Lorin patents a design for the ramjet engine.
Data from Junkers aircraft and engines, 1913-1945, Junkers: an aircraft album General characteristics Length: 7.12 m (23 ft 4 in) Wingspan: 10 m (32 ft 10 in) Height: 2.39 m (7 ft 10 in) Wing area: 13.7 m 2 (147 sq ft) Empty weight: 340 kg (750 lb) Gross weight: 590 kg (1,301 lb) Fuel capacity: 95 L (25 US gal; 21 imp gal) Powerplant: 1 × Armstrong Siddeley Genet II five-cylinder air-cooled ...
The Armstrong Siddeley Screamer was a British rocket engine intended to power the Avro 720 manned interceptor aircraft (Avro's competitor to the Saunders-Roe SR.53 for a rocket-powered interceptor). Thrust was variable, up to a maximum of 8,000 lbf (36 kN).