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The Bristol Mercury VIII was
an air-cooled radial aircraft engine with nine cylinders. It was rated
at 840 hp (626 kW). Derived from the Jupiter, it had a bore of 5.75
inches (146mm) and stroke of 6.5 inches (165mm). The relatively short
stroke reduced the engine diameter significantly from the Jupiter.
Aircraft using this engine included the Blenheim.
References
Gunston (2006)
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