M-82A Aircraft Engine,Technical Specifications (USSR)

M-82A Aircraft Engine Technical Specifications

  • Working volume-41.2 liters
  • Compression ratio-7.05
  • Power – 1530 hp
  • Weight-870 kg
  • Diameter-1260 mm
  • Cylinder diameter-155.5 mm
  • Take-off power – 1700 hp

M-82A Aircraft Engine Details

Aviation star-shaped 14-cylinder double-row air-cooled engine, manufactured in 1941. The M-82 aircraft engine was found on the battlefield in the Murmansk region and donated to the museum by the head of the Aviation Restoration Group LLC, O. Y. Leiko.

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