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  2. Zanzottera MZ 201 - Wikipedia

    en.wikipedia.org/wiki/Zanzottera_MZ_201

    The engine was originally designed and produced by Zanzottera Technologies of Italy, but the design was sold, along with the rest of the company's two-stroke ultralight aircraft engine line, to Compact Radial Engines of Surrey, British Columbia, Canada. [3]

  3. Zanzottera MZ 301 - Wikipedia

    en.wikipedia.org/wiki/Zanzottera_MZ_301

    The Zanzottera MZ 301 is a three-cylinder, in-line two-stroke, dual ignition aircraft engine designed for ultralight aircraft. [1] [2]The engine was originally designed and produced by Zanzottera Technologies of Italy, but the design was sold, along with the rest of the company's two-stroke ultralight aircraft engine line, to Compact Radial Engines of Surrey, British Columbia, Canada. [2]

  4. 2si 460 - Wikipedia

    en.wikipedia.org/wiki/2si_460

    The 2si 460 is a family of in-line twin-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by ILO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.

  5. 2si 540 - Wikipedia

    en.wikipedia.org/wiki/2si_540

    The 2si 540 and 2si 500 are a family of in-line twin-cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft. [1]The basic engine was originally designed and produced by JLO-Motorenwerke of Germany and was later acquired by the AMW Cuyuna Engine Company of Beaufort, South Carolina and marketed under the Cuyuna brand name.

  6. Rotax 912 - Wikipedia

    en.wikipedia.org/wiki/Rotax_912

    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.

  7. Rotax 503 - Wikipedia

    en.wikipedia.org/wiki/Rotax_503

    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 ...