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Data from Bayerl and the manufacturer General characteristics Crew: one Capacity: one passenger Length: 4.78 m (15 ft 8 in) Width: 1.73 m (5 ft 8 in) Height: 2.74 m (9 ft 0 in) Airfoil: NACA 8-H-12 Empty weight: 265 kg (584 lb) Gross weight: 450 kg (992 lb) Fuel capacity: 86 litres (19 imp gal; 23 US gal) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft ...
The ArrowCopter was designed to comply with British BCAR Section T rules. It features a single main rotor, a two-seats in tandem configuration enclosed cockpit with a bubble canopy, stub wings, tricycle landing gear and a four-cylinder, liquid and air-cooled, four-stroke, dual-ignition turbocharged 115 hp (86 kW) Rotax 914 engine in pusher configuration.
The Cavalon is a two-seats-in-side-by-side configuration development of the tandem-seating AutoGyro Calidus.It features a single main rotor, an 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 or 135 ...
Subsequently, production of autogyros was licensed to several manufacturers, including the Pitcairn Autogiro Company in the United States and Focke-Wulf of Germany. A Focke-Wulf-built Cierva C.19 Mk.IV Autogiro. In 1927, German engineer Engelbert Zaschka invented a combined helicopter and autogyro. The principal advantage of the Zaschka machine ...
AutoGyro Cavalons AutoGyro Calidus. AutoGyro GmbH (English: AutoGyro Limited) is a German aircraft manufacturer based in Hildesheim.The company specializes in the design and manufacture of autogyros in the form of fully assembled, ready to fly aircraft.
The CarterCopter is an experimental compound autogyro developed by Carter Aviation Technologies in the United States to demonstrate slowed rotor technology. On 17 June 2005, the CarterCopter became the first rotorcraft to achieve mu-1 (μ=1), an equal ratio of airspeed to rotor tip speed, [3] but crashed on the next flight [1] and has been inoperable since. [4]
The SkyCruiser features a single main rotor, a two-seats-in tandem open cockpit with a windshield, tricycle landing gear with wheel pants, plus a tail caster and a four-cylinder, liquid and air-cooled, four stroke 115 hp (86 kW) Rotax 914 turbocharged engine or modified 125 hp (93 kW) turbocharged Rotax 912 in pusher configuration.
The G1SA Genesis Solo features a single main rotor, a single-seat open cockpit with a windshield, tricycle landing gear with wheel pants, plus a tail caster and a twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration.