Scorpion I is a piston engine model used in aircraft.
Engine Family: piston
Compression ratio: 4
Bore: 87.5 millimetre
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 2
Displacement: 1100 cubic-centimetre
Dry weight: 41 kilogram
Fuel grade: 74
Fuel type: Avgas
Max. continuous RPM: 2300
Max. continuous hp: 34 horsepower
Max. takeoff RPM: 2500
Max. takeoff hp: 30 horsepower
Stroke: 91.5 millimetre
