Hirth HM 508
From Wikipedia, the free encyclopedia
The Hirth HM 508 was an air-cooled, eight-cylinder, inverted-V aircraft engine built in Germany in the 1930s. It had a bore and stroke of 105 mm × 115 mm (4.1 in × 4.5 in) and developed 210 kW (280 hp) at 3,000 rpm.
[edit] Applications
[edit] References
Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens, 75.
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