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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.
Data from Jane's All the World's Aircraft 2010/11 [1] except where specified. M-16 Tandem Trainer Initial version. Normally powered by a Rotax 914UL, but a 74 kW (99 hp) Rotax 912 ULS may be fitted. Introduced 2000. M-16-2006 Tandem Trainer Improved lubrication, cooling, centre of gravity position and avionics. Introduced 2006. M-19 Shark
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 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 ...
The ELA 10 Eclipse has a single main rotor, a two-seats-in tandem enclosed cockpit with a bubble canopy, tricycle landing gear with wheel pants, plus a tail caster and a four-cylinder, liquid and air-cooled, four stroke 100 hp (75 kW) Rotax 912 ULS or turbocharged 115 hp (86 kW) Rotax 914 engine in pusher configuration.
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.
Data from Jane's All the World's Aircraft 2010/11 General characteristics Crew: two Length: 12 ft 3 in (3.73 m) fuselage Width: 6 ft 1 in (1.85 m) fuselage maximum Height: 10 ft 0 in (3.05 m) overall Empty weight: 899 lb (408 kg) Gross weight: 1,499 lb (680 kg) Fuel capacity: 87 L (19.2 Imp gal, 23.0 US gal) usable Powerplant: 1 × Subaru EJ25 flat four piston, 160 hp (119 kW) Main rotor ...
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]