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The first fuel injected 22R-E engines appeared in August 1982. Output of these engines is commonly rated at 78 kW (105 hp; 106 PS) at 4,800 rpm and 185 N⋅m (136 lb⋅ft) at 2,800 rpm. In 1985, the engine was significantly reworked, output was up to 84 kW (113 hp; 114 PS) at 4,800 rpm and 190 N⋅m (140 lb⋅ft) at 3,600 rpm.
TSR-2 with Olympus Mk.320 engines on display at the Royal Air Force Museum Cosford. The performance specification for the BAC TSR-2 was issued in 1962. It was to be powered by two BSEL Olympus Mk 320 (BOl.22R) engines each rated at 19,610 lbf (87.2 kN) dry and 30,610 lbf (136.2 kN) with reheat at take-off.
The initial design of the engine was a civil version of the Olympus 22R, redesignated as the 591. [1] The 22R had been designed for sustained (45 minutes) flight at Mach 2.2 [3] as the engine for the BAC TSR-2. The 591 was redesigned, being known as the 593, with specification finalised on 1 January 1964. [1]
The use of "G" to denote twin cam engines was decided on in 1971, with the renaming of the 10R into 8R-G. Before that, twin cams had received separate numerical codes. [1] In 1987, Toyota began assigning dual letter engine codes to some of the "engine family" categories in some engine lines, particularly six-cylinder models.
Fuel injection became standard on all North American Celicas started from August 1982, therefore the 22R engine became 22R-E (or 22R-EC with California emissions equipment). In August 1982, Toyota added the GT-S model to the North American market to re-inject the sports image that Celica had lost as it grew larger and heavier with each ...
The Bristol design was the Type 172 and was to be powered by four or six Bristol engines of 9,000 lbf (40 kN) thrust [7] to the Ministry engine specification TE.1/46. The thrust required of the new engine, then designated B.E.10 (later Olympus), would initially be 9,000 lbf (40 kN) with growth potential to 12,000 lbf (53 kN).