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Armstrong Siddeley Cheetah Engine
The Armstrong Siddeley
Cheetah is a mid
range 7-cylinder air-cooled
295 horsepower radial engine,
and is a pre-war and wartime product of the British Armstrong Siddeley
company. The Cheetah engine was designed by Armstrong Siddeley in 1930 and had evolved from the 7 cylinder Lynx radial of 1920 originally being known as the Lynx Major. It was used
primarily on prewar British military aircraft,
including the Avro 626 biplane trainer and most
significantly the Avro Anson monoplane bomber which in 1935 was Britains
first twin engined aircraft with retractable undercarriage, achieving a
production run of over 10,000 airframes in England and Canada.
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7-Cylinder air-cooled radial poppet valve direct drive engine |
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Bore x Stroke 5.3 x 5 inches (133 x 127 mm) |
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Swept Volume 834 cubic inches (13.7 litres) |
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|Maximum Power 355 horsepower @ 2,425 rpm |
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Weight 556 lbs. (253 Kg) |
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Carburetor fuel system (with centrifugal supercharger) |
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