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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. Zanzottera MZ 34 - Wikipedia

    en.wikipedia.org/wiki/Zanzottera_MZ_34

    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]

  5. Rotax 447 - Wikipedia

    en.wikipedia.org/wiki/Rotax_447

    The Rotax 447 is a 41.6 hp (31 kW), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft. [1] [2]

  6. Ultralight aviation - Wikipedia

    en.wikipedia.org/wiki/Ultralight_aviation

    Huntair Pathfinder Mark 1 ultralight. Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons, elevator and rudder, calling the former "microlight" and the latter "ultralight".

  7. 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.

  8. Zenoah G-25 - Wikipedia

    en.wikipedia.org/wiki/Zenoah_G-25

    The engine runs on a mixture of unleaded auto fuel and oil. [1] [2] Producing 22 hp (16 kW) at 6600 rpm, the G-25 competed in the early 1980s ultralight powerplant market against the similar Rotax 277. Production of the engine was completed in the late 1980s and today only used engines and parts are available. [1] [2]

  9. Rotax 582 - Wikipedia

    en.wikipedia.org/wiki/Rotax_582

    The Rotax 582 is based upon the earlier Rotax 532 engine design and was designed for ultralight aircraft. [ 4 ] [ 5 ] The 582 increased the bore from the 532 engine's 72 to 76 mm (2.8 to 3.0 in). This increased the displacement from 521.2 cc (31.81 cu in) to 580.7 cc (35.44 cu in), an increase of 11%.

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