| Rotorvox C2A | |
|---|---|
 | |
| Role | Two seat autogyro |
| National origin | Germany |
| Manufacturer | Rotorvox GGC GmbH |
| First flight | c.2009 |
The Rotorvox C2A is a two-seat, pusher configuration autogyro developed in Germany.
| Rotorvox C2A | |
|---|---|
| | |
| Role | Two seat autogyro |
| National origin | Germany |
| Manufacturer | Rotorvox GGC GmbH |
| First flight | c.2009 |
The Rotorvox C2A is a two-seat, pusher configuration 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 three blade propeller. The rotor is pre-rotated hydraulically. [1]
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. [1]
At least two prototypes were flown over five years of development before C2A deliveries began in October 2014. [1]
Data from Jane's All the World's Aircraft 2015/16 p.279 [1]
General characteristics
Performance
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