Search results
Results from the WOW.Com Content Network
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.
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.
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 ...
Print/export Download as PDF; Printable version; In other projects Appearance. move to sidebar hide. From Wikipedia, the free encyclopedia ... org/w/index.php?title ...
EASA type-certified model in the CS-LSA category. Short wing version powered by a 100 hp (75 kW) Rotax 912 S3 engine. [11] Virus SW 600 D Based on the SW 121 but featuring a 100 hp (75 kW) Rotax 912 ULS engine, it is the first aircraft to be certified under the new German LTF-UL2019 rules for the 600 kg microlight category. [22]
A 74 kW (99 hp) Rotax 912 ULS is the standard powerplant but there are other options such as the 60 kW (80 hp) Rotax 912 UL or the Jabiru 2200 and Jabiru 3300 engines of similar power. [ 3 ] One significant modification of the Breezer prototype after its first year of test flying was the incorporation of a steerable nosewheel in place of a ...
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 ...
Version of the CTLS introduced in 2012 and powered by a Rotax 912 iS engine of 100 hp (75 kW). This fuel-injected engine reduces fuel consumption by 21% compared to the carbureted versions. The model has a $12,800 higher price, but that includes the new engine, electric trim and a lithium ion battery.