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The Rotax 912 is a horizontally-opposed four-cylinder, naturally-aspirated, four-stroke aircraft engine with a reduction gearbox. It features liquid-cooled cylinder heads and air-cooled cylinders. Originally equipped with carburetors , later versions are fuel injected .
Moving towards more demanding aircraft applications, Rotax, by 1989, developed a four-stroke, four-cylinder, engine: the Rotax 912, with versions eventually ranging from 60 to 75 kW (80 to 100 hp), followed by a turbocharged 115 horsepower Rotax 914. [5]
The mid-model, which adds an instrument pod, wheel pants, a retractable wing-mounted pylon with a gas strut, pylon fairing, extra stowage and powered by the Rotax 582, twin cylinder, two-stroke, liquid-cooled engine of 48 kW (64 hp). Price in 2000 was US$16,500 ready to fly. [1] [2] Quantum SuperSport/Quantum 912
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.
Pipistrel Sinus 912 Sinus 447 Rotax 447 powered variant for the Slovenian market. Sinus 503 Rotax 503 powered variant with a variable-pitch folding propeller. Sinus 582 As the 503 but fitted with a Rotax 582. Sinus 912 Rotax 912 powered variant in either UL, LSA or experimental version. [8] [13] Sinus FLEX Sinus 912 variant with interchangeable ...
Pages in category "Rotax engines" The following 17 pages are in this category, out of 17 total. ... Rotax 535; Rotax 582; Rotax 618; Rotax 912; Rotax 914; Rotax 915 iS;
Powerplant: 1 × Rotax 912 ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 73.5 kW (98.6 hp) Performance. Maximum speed: 176 km/h (109 mph, 95 kn)
Data from Jane's All the World's Aircraft 2011-12 General characteristics Capacity: 2 Length: 5.78 m (19 ft 0 in) Wingspan: 9.78 m (32 ft 1 in) Height: 2.8 m (9 ft 2 in) Wing area: 14.62 m 2 (157.4 sq ft) Empty weight: 278 kg (613 lb) including parachute Max takeoff weight: 450 kg (992 lb) Fuel capacity: 59 L (13 Imp gal, 15.6 US gal) Powerplant: 1 × Rotax 912 UL 4-cylinder horizontally ...