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Dynamic, turbocharged iS engine with best power-to-weight ratio and TBO 2,000h. Four-stroke piston engine with four liquid and air-cooled cylinders. Redundant electronic fuel injection and ignition, eco mode. Turbocharger, stainless steel exhaust.
- Launch Configurator
ROTAX 916 i. 160 HP. iS A / iSc A / iS C24 / iSc C24. 1....
- iSc C24
Rotax Aircraft Engines Imagebrochure pdf Documentazione...
- 914 UL
Low-weight engine with excellent performance at high...
- Launch Configurator
Dynamic iS engine with best power-to-weight ratio. Four-stroke piston engine with four liquid and air-cooled cylinders. Redundant electronic fuel injection and ignition, eco mode. Turbocharger, stainless steel exhaust. Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets.
The Rotax 914 is a turbo-charged, four-stroke, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads. It is designed and built by the Austrian company BRP-Powertrain, owned by Bombardier Recreational Products (BRP), as part of its Rotax brand.
The most powerful 2-stroke turbo snowmobile engine ever from a factory. Heart-pounding power and response is at your fingertips take the ride further than ever before. Pumping 180 horsepower* up to 8,000 feet and maintaining a massive advantage over natrually aspirated 850-cc engines as altitude increases, and built for the ultimate ride on the ...
Low-weight engine with excellent performance at high altitudes. Four-stroke piston engine with four liquid and air-cooled cylinders. Turbocharger. Automatic wastegate control. Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet. 2 carburetors.
The Rotax 916 iS is an Austrian piston aircraft engine, designed and produced by Rotax of Gunskirchen for use in light aircraft, light sport, ultralight, homebuilt aircraft and Unmanned aerial vehicle.
The Rotax 915 iS is a four-cylinder four-stroke, horizontally-opposed, turbocharged, air and liquid-cooled, gasoline engine design, with a mechanical gearbox reduction drive. The turbocharger has a compression ratio of 3.5:1 and the engine will have a critical altitude of 15,000 ft (4,572 m).
