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Fuel type: gasoline minimum MON 85, RON 95, AKI 91, leaded or unleaded, avgas 100LL, maximum ethanol 10% Oil system: dry sump, forced lubrication with separate oil tank Cooling system: air cooled with liquid cooled cylinder heads
The Rotax 915 iS is an Austrian aircraft engine, produced by Rotax of Gunskirchen for use in ultralight aircraft, homebuilt aircraft, light-sport aircraft, small helicopters and gyroplanes. The engine was type certified in 2017. [2] [3] The engine was first publicly displayed at AirVenture in July 2015 [2] and first flown in March 2016. [4]
The Ikarus C42 is a single-engined high-wing monoplane with side-by-side seats for two in a 1.22 m (48 in) wide cabin. The C42 is manufactured with either an 80 hp (60 kW) Rotax 912 engine or a 100 hp (75 kW) Rotax 912s engine. The Rotax engine has a low fuel consumption and relatively low noise.
The fuel consumption per mile or per kilometre is a more appropriate comparison for aircraft that travel at very different speeds. [citation needed] There also exists power-specific fuel consumption, which equals the thrust-specific fuel consumption divided by speed. It can have units of pounds per hour per horsepower.
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. [3] [4] [5]
The RV-12iS is an incremental improvement over the RV-12 which allows the installation of the Rotax 912ULS (carbureted) or the Rotax 912iS (fuel-injected) engines. It also incorporates a new cowling and throttle quadrant design, quick-retracting flaps, a quick-adjusting seat, redesigned landing gear attachments and fuel tank, among other ...
Fuel capacity: 96 litres (21 imp gal; 25 US gal) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (101 hp) Propellers: 3-bladed constant speed propeller
It is the rate of fuel consumption divided by the power produced. In traditional units, it measures fuel consumption in pounds per hour divided by the brake horsepower, lb/(hp⋅h); in SI units, this corresponds to the inverse of the units of specific energy, kg/J = s 2 /m 2. It may also be thought of as power-specific fuel consumption, for ...