Praga D

From Wikipedia, the free encyclopedia

The Praga D was a four-cylinder, air-cooled, horizontally-opposed aircraft engine first produced in Czechoslovakia in 1936 but which enjoyed its greatest success after World War II due to the explosion in popularity of sports flying.

[edit] Specifications

  • Bore: 95 mm (3.7 in)
  • Stoke: 100 mm (3.9 in)
  • Displacement: 2.83 L (173 cu in)
  • Power: 56 kW (75 hp) at 2,650 rpm

[edit] References

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