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Rotorvox C2A
The Rotorvox C2A is a two-seat autogyro developed in Germany.
Structurally, the C2A is largely carbon-fibre monocoque. The fuselage pod contains a protective cell for the side-by-side seating behind a large, forward hinged, three piece canopy. A faired pylon, mounted immediately behind the cell supports a two blade aluminium rotor and behind it a 73 kW (98 hp) Rotax 914 liquid-cooled flat-four engine drives a pusher three blade propeller. The rotor is pre-rotated hydraulically.
Flat-sided tail booms are held away from the fuselage on short stubs and each mounts a straight-tapered fin and rudder, their tips linked by the tailplane. There are shallow, long ventral fins. The C2A has a short-legged, wide track tricycle undercarriage with its mainwheels near to the forward end of the booms and a nosewheel under the forward fuselage.
First flown around 2009, at least two prototypes were flown over five years of development before C2A deliveries began in October 2014.
Engine: 1 × Rotax 914, 73 kW (98 hp) continuous
Main rotor diameter: 8.40 m (27 ft 7 in)
Blades: two aluminium, airfoil NACA 8H12
Length: 5.50 m (18 ft 1 in) fuselage; including rotors 8.40 m (27 ft 7 in)
Width: 2.21 m (7 ft 3 in) fuselage
Height: 2.85 m (9 ft 4 in)
Max takeoff weight: 560 kg (1,235 lb)
Fuel capacity: 90 l (20 imp gal; 24 US gal)
Propellers: 3-bladed Duc, 1.75 m (5 ft 9 in) diameter
Cruise speed: 145 km/h (90 mph; 78 kn)
Never exceed speed: 164 km/h (102 mph; 89 kn)
Range: 600 km (373 mi; 324 nmi)
Endurance: maximum 6 hr
Crew: Two
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