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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 80 hp (60 kW) 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.
Between 1985 and 1995, 60,000 Rotax engines were sold for aircraft propulsion. [2] In the light aircraft class, in 1998 Rotax outsold all other aero engine manufacturers combined. [4] Their four-stroke engines powered most U.S.-certified light sport aircraft when they first appeared around 2004. [5]
Category: Rotax engines. 1 language. ... Rotax Max This page was last edited on 21 December 2016, at 06:54 (UTC). Text is available under the Creative ...
Standard engine is the 100 hp (75 kW) Rotax 912ULS and the 2010 base price is US$99,000. [16] S-6S Super Six Improved version with dope and fabric covering, introduced in 1993. Standard engine is the 100 hp (75 kW) Rotax 912ULS. Available with standard wing, "116" wing and "light sport wing". In production in 2010. [3] [5] [6] [13]
The Rotax 535 is an Austrian aircraft engine, that was designed and produced by Rotax of Gunskirchen for use in motor gliders. [1] The first application for type certification to JAR 22, Appendix H, was made on 29 June 1982 and the first certification was granted on 27 April 1983. [1] It is out of production and is no longer offered for sale by ...
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 ...
The Rotax 503 is a 37 kW (50 hp), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft. [ 1 ] [ 2 ] For decades the engine was one of the most popular and reputedly reliable aircraft engines in its class (two-stroke, under 60 horsepower), [ 3 ] and it remains widely used and ...
Data from OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582 General characteristics Type: two-stroke air-cooled aeroengine Bore: 67.5 mm (2.66 in) Stroke: 61 mm (2.4 in) Displacement: 426.5 cc (26.64 cu in) Dry weight: 26.8 kg (59 lb) (dry, no exhaust system) Components Valvetrain: piston ports Fuel system: pneumatic pump pressurized Fuel type: regular autofuel Oil system: premixed in the fuel ...
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