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The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 60 kW (80 hp) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.
Version powered by a 48 kW (64 hp) Rotax 582 engine. Price in 2003 was £16,450. [2] Blade 912 Version powered by a 60 kW (80 hp) Rotax 912UL or the 74.5 kW (100 hp) Rotax 912ULS. In 2003 it was reported that the Blade 912 accounted for the majority of customer orders. Price in 2003 was £21,800. [2]
Skyranger Original model, introduced 1990. [2]Skyranger Vfun Renamed original model for the Fédération Aéronautique Internationale microlight class. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke, the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS, 85 hp (63 kW) Jabiru 2200, the 60 to 80 hp (45 to 60 kW) VW and the 60 hp (45 kW) HKS 700E four-stroke ...
By 2014, Rotax had produced and sold 50,000 of 912/914 four-stroke engines. [5] Later models increased power, with several variants of the 912 family, and a new 100 kW (135 hp) Rotax 915 iS . [ 5 ] [ 20 ]
Tornado II 912 Two seats in tandem version, intended for the US homebuilt category. It has a 23.5 ft (7.2 m) wingspan. Standard engine is the 80 hp (60 kW) Rotax 912 and cruise speed is 120 mph (193 km/h) with that engine. Acceptable power range is 52 to 80 hp (39 to 60 kW).
Data from Lockwood Aircraft & Kitplanes General characteristics Crew: one Capacity: one passenger and 505 lbs (229 kg) useful load Length: 22 ft 0 in (6.71 m) Wingspan: 30 ft 0 in (9.15 m) Height: 10 ft 0 in (3.05 m) Wing area: 160 sq ft (14.88 m 2) Empty weight: 495 lb (224 kg) Max takeoff weight: 1,000 lb (454 kg) Powerplant: 1 × Rotax 912 UL four stroke piston engine, 80 hp (60 kW ...
Standard engines available are the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS and the 120 hp (89 kW) Jabiru 3300 four-stroke powerplants. [1] [2] A Magnum 501 rocket powered parachute system is under development for the aircraft. [4] [5] The Alto TG design was issued a Czech type certificate on 15 July 2008 and produced until ...
Improved model powered by a 64 hp (48 kW) Rotax 582 or 80 hp (60 kW) Rotax 912UL engine. Can accept engines from 65 to 210 hp (48 to 157 kW). Can accept engines from 65 to 210 hp (48 to 157 kW). Empty weight is 350 lb (159 kg) and gross weight is 760 lb (345 kg).
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