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  2. AAI Sparrowhawk - Wikipedia

    en.wikipedia.org/wiki/AAI_Sparrowhawk

    The two-bladed rotor is of bonded metal construction. [1] The tail unit is attached by a pair of aluminum centreline booms. The upper one is mounted directly on the vertical engine/rotor mast and is cranked near midpoint to clear the propeller tips. The lower one is attached well below the keel on an extension plate.

  3. AutoGyro Calidus - Wikipedia

    en.wikipedia.org/wiki/AutoGyro_Calidus

    The Calidus features a single main rotor, a two-seats in tandem enclosed cockpit with a complete aerodynamic cockpit fairing, tricycle landing gear with wheel pants and a four-cylinder, air and liquid-cooled, four-stroke, dual-ignition 100 hp (75 kW) Rotax 912 engine or turbocharged 115 hp (86 kW) Rotax 914 engine in pusher configuration.

  4. Cicaré CH-8 - Wikipedia

    en.wikipedia.org/wiki/Cicaré_CH-8

    The piston engine-powered CH-8 ultralight series use the traditional "penny-farthing" layout with two-bladed main and tail rotors. The main rotor is formed from composites and is a teetering, semi-rigid design with 6° of twist. The pod-and-boom fuselage has a carbon fiber and epoxy resin cabin with a long transparent forward-opening canopy.

  5. Vortech G-1 - Wikipedia

    en.wikipedia.org/wiki/Vortech_G-1

    The aircraft was designed long before the adoption of the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg), but nonetheless complies with them. The aircraft has a standard empty weight of 150 lb (68 kg) and is billed as the "World's Tiniest Homebuilt Helicopter" by the plans supplier.

  6. Helowerks HX-1 Wasp - Wikipedia

    en.wikipedia.org/wiki/Helowerks_HX-1_Wasp

    The Wasp is a traditional pod and boom helicopter with a twin-blade rotor powered by a 90shp (97 kW) Garrett JFS-100-13A turboshaft engine. [1] It has a fixed skid landing gear and enclosed cabin with two-seat side-by-side seats. [1]

  7. EDM Aerotec CoAX 2D/2R - Wikipedia

    en.wikipedia.org/wiki/EDM_Aerotec_CoAX_2D/2R

    The CoAX 2D/2R was originally known as the FLIP 2 (Fly In Perfection) and is a derivative of the FLIP 1, a conventional helicopter with a main and tail rotor.[1]The CoAX 2D/2R was designed to comply with the European Class 6 microlight helicopter rules, including the category's maximum takeoff weight of 450 kg (992 lb).

  8. List of ultralight helicopters - Wikipedia

    en.wikipedia.org/wiki/List_of_ultralight_helicopters

    Voytovich helicopter Ukraine [31] Kazachok Helicopter Russia [32] Kazan Aktai: Russia Rotorfly Russia [33] Berkut (helicopter) Russia FLY CC III Czech Republic [34] jpkrucker Canada Single seat coaxial heli [35] Mosquito XE: Canada / United States Hungarocopter HC-01: Hungary [36] Hungarocopter HC-02: Hungary [37] CoaX helicopters Australia [38 ...

  9. Heli-Sport CH-7 - Wikipedia

    en.wikipedia.org/wiki/Heli-Sport_CH-7

    In 1989 EliSport, which became Heli-Sport in 1997, bought the rights to the Cicare CH-6, a small single-seat open cockpit helicopter designed in Argentina by Augusto Cicaré. It was developed by Josi and Claudio Barbero and, with the help of the sports car designer, Marcello Gandini who produced a new, enclosed cabin, marketed from 1992 as the ...