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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 Trixy G 4-2 R ("Gyro For Two powered by Rotax") is an Austrian autogyro, designed and produced by Trixy Aviation Products of Dornbirn. The aircraft was introduced at the Aero show held in Friedrichshafen in 2011 and when it was available it was supplied as a complete ready-to-fly-aircraft.
The gyroplane was designed to comply with the US Experimental - Amateur-built rules. It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear , and a twin cylinder, two-stroke , liquid-cooled, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration .
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 Monarch was designed to comply with the US Experimental - Amateur-built rules. It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear with wheel pants and a twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration.
Magni Gyro currently produces five sport autogyro models, all with similar pod and low boom, pusher engine layouts and the M-24 Orion have side by side seating and an enclosed cabin. It has a steel airframe with a carbon fibre cabin and engine-enclosing pod. Transparent, top hinged doors on either side give access to the two seats, which are ...
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 Fairey Rotodyne was a 1950s British compound gyroplane designed and built by Fairey Aviation and intended for commercial and military uses. [1] A development of the earlier Fairey Jet Gyrodyne, which had established a world helicopter speed record, the Rotodyne featured a tip-jet-powered rotor that burned a mixture of fuel and compressed air bled from two wing-mounted Napier Eland turboprops.