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G75 75kW Water-Cooled Four-Stroke Gasoline Piston Engine For UAV And Low-Altitude Aircraft

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Product Overview

Technical Specifications

Structure Four-stroke, four-cylinder boxer
Cooling System Water cooling
Reduction Gear Direct drive
Control Unit ECU
Ignition System Dual CDI
Generator 300W / 25A
Cylinder Diameter 103 mm
Stroke 80 mm
Displacement 2,697 cc
Compression Ratio 8.0
Power 75 kW
Dry Weight 55 kg
Fuel Type Gasoline 95#
Lubrication Dry sump

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