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The engine is a V-twin four-stroke, 895 cc (54.6 cu in) or 993 cc (60.6 cu in) displacement, fan-driven air-cooled, gasoline engine design.The larger displacement is achieved by increasing the stroke from 78 to 87 mm (3.1 to 3.4 in), but using the same bore of 86 mm (3.4 in).
The engine was also used in two variants of the Vanguard. The Sportsman was a high-performance version made in 1956 and 1957 with two SU carburettors and a compression ratio of 8:1, yielding 90 hp (67 kW) at 4500 rpm. The Ensign was an economy version introduced in 1957.
At the top of the range was the Standard Flying V-Eight, with a 20 RAC hp side-valve 90 degree V8 engine and a top speed of more than 80 mph (130 km/h). 250 Flying V-Eights were made from 1936 to 1937; they were offered for sale from 1936 to 1938 with the initial price of £349 lowered to £325 in the last year to clear inventory. [10]
It was used to power the first stage of the Vanguard rockets on the Vanguard project. As was common to engines based on the V-2 experience, the turbine was driven by steam generated by catalytic decomposition of H 2 O 2 and the combustion chamber was regeneratively cooled. [3] [4] The engine was gimbaled to supply thrust vectoring.
The chassis was stiffened to take the weight of the heavier engine and performance suffered with 65 mph (105 km/h) about the top speed. Like the petrol engines, the diesel was a Standard-built "20C" engine developed for the Ferguson tractor. The diesels fitted to the tractor were restricted to 2200 rpm and developed 25 horsepower (19 kW), but ...
From 1985 to 1988 the company manufactured the Standard 2000, a version of the Rover SD1 powered by a 2 L (2,061 cc) Standard four-cylinder engine borrowed from an old Standard Vanguard model (as also used in the Standard 20 commercial vehicle). Power was a mere 83 hp (62 kW) at 4,250 rpm.