Beskrivning
Art.nr: 23231
The price of the product is without VAT
The Roto 125 FSi is a new engine for inline engine aircraft. The design of the engine was aimed at easy installation in an aircraft with a narrow fuselage. Engine performance is comparable to 125cc four-stroke engines, low idle and easy starting is a given.
The engine has been developed with all the experience provided from the Roto - UAV development group and meets the highest possible standards of production quality and output testing.
The Roto 125 FSi is a twin cylinder, four stroke, air cooled inline engine with a single carburettor for ease of user setup. The engine is completely built on roller bearings and is completely maintenance free. Engine lubrication is provided by a system adopted from Roto - UAV and no relubrication is required. The valves and their gears are developed so that their inspection is not necessary before 40 hours of operation.
Technical data:
Engine displacement: 125 ccm
Power: 7,5 kW
Max static engine thrust: 21 kg
Bore: 2x48 mm
Engine weight: 4300 g
Engine & ignition weight: 4580 g
Arrangement of the engine: inline two-cylinder
Cooling: air-cooled
Lubrication: petrol 95 oct. + 2% oil
RPM: 1100 6000
Fuel system: Carburettor
The Roto 125 FSi is a new engine for inline engine aircraft. The design of the engine was aimed at easy installation in an aircraft with a narrow fuselage. Engine performance is comparable to 125cc four-stroke engines, low idle and easy starting is a given.
The engine has been developed with all the experience provided from the Roto - UAV development group and meets the highest possible standards of production quality and output testing.
The Roto 125 FSi is a twin cylinder, four stroke, air cooled inline engine with a single carburettor for ease of user setup. The engine is completely built on roller bearings and is completely maintenance free. Engine lubrication is provided by a system adopted from Roto - UAV and no relubrication is required. The valves and their gears are developed so that their inspection is not necessary before 40 hours of operation.
Technical data:
Engine displacement: 125 ccm
Power: 7,5 kW
Max static engine thrust: 21 kg
Bore: 2x48 mm
Engine weight: 4300 g
Engine & ignition weight: 4580 g
Arrangement of the engine: inline two-cylinder
Cooling: air-cooled
Lubrication: petrol 95 oct. + 2% oil
RPM: 1100 6000
Fuel system: Carburettor