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  2. Flying K Sky Raider - Wikipedia

    en.wikipedia.org/wiki/Flying_K_Sky_Raider

    Stretched version with two seats in tandem, a gross weight of 950 lb (431 kg), an acceptable power range of 60 to 80 hp (45 to 60 kW). Engines used include the two-stroke 50 hp (37 kW) Rotax 503 and the four-stroke 60 hp (45 kW) HKS 700E engine. Described as an "intimate tandem two seater" due to the small rear seat space. Production completed.

  3. Fin Komodo - Wikipedia

    en.wikipedia.org/wiki/Fin_Komodo

    The first prototype was designed with a single seat while the second prototype was designed with 2 chairs. Both of these prototypes had an oil capacity of 0.3 liters, fuel capacity of 15 liters of gasoline, used a seamless tubular frame and trunk, and generated torques of 1.19 kg / 3000 rpm (11.7 Nm / 3000 rpm).

  4. List of ultralight helicopters - Wikipedia

    en.wikipedia.org/wiki/List_of_ultralight_helicopters

    Coaxial Single Seater [19] Coaxial heli Zhuzhou China Coaxial Single Seater [20] Agricultural coaxial heli China [21] Red Coaxial Helicopter China Coaxial Single Seater [22] White Coaxial Chopper China Coaxial Single Seater [23] Homebuilt Coaxial Heli China Coaxial Single Seater [24] Yellow tail coaxial heli China [25] Famà Kiss 209: Italy Sk ...

  5. Eipper Quicksilver - Wikipedia

    en.wikipedia.org/wiki/Eipper_Quicksilver

    Quicksilver MX Quicksilver MX II Sprint two seater Quicksilver Sport 2S, showing its struts, in place of wire bracing Quicksilver C The C model was the earliest powered version and consisted of the Quicksilver hang glider, including the weight-shift sling seat, with a McCulloch MAC 101 powerplant of 12 hp (9 kW), a V-belt reduction drive and a 1.7 US gal (6 L) fuel tank.

  6. Phantom X1 - Wikipedia

    en.wikipedia.org/wiki/Phantom_X1

    Data from Kitplanes General characteristics Crew: one Length: 16 ft 8 in (5.08 m) Wingspan: 28 ft 6 in (8.69 m) Height: 8 ft 2 in (2.49 m) Wing area: 142 sq ft (13.2 m 2) Empty weight: 250 lb (113 kg) Gross weight: 510 lb (231 kg) Fuel capacity: 5 US Gallons (19 litres) Powerplant: 1 × Rotax 447 twin-cylinder, single-ignition, two-stroke aircraft engine, 40 hp (30 kW) Performance Maximum ...

  7. Rans S-4 Coyote - Wikipedia

    en.wikipedia.org/wiki/Rans_S-4_Coyote

    The Coyote S-4 has conventional landing gear, while the S-5 has tricycle gear. Both can be equipped with floats and skis. The original basic engine was the Rotax 277 of 28 hp (21 kW), with the Rotax 447 of 40 hp (30 kW) and the Rotax 503 of 50 hp (37 kW) available later as options. [1] [2] [11] The Coyote II two-seater was later developed from ...