Rotorvox C2A
Rotorvox GGC GmbH · Germany · first flew 2009 · light aircraft
The Rotorvox C2A is a German two-seat pusher autogyro with a largely carbon-fibre monocoque fuselage.
Recognition (WEFT)
| W — Wings | High-mounted, rotary |
|---|---|
| E — Engines | 1 × piston, fuselage-mounted |
| F — Fuselage | 5.5 m fuselage |
| T — Tail | Twin fin |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Pusher autogyro with a two-blade aluminium rotor on a faired pylon
- Twin tail booms with fins and rudders linked at their tips by the tailplane
- Carbon-fibre pod with side-by-side seating under a large forward-hinged canopy
A pod-shaped pusher autogyro with twin tail booms joined by a tailplane, short ventral fins and a wide-track tricycle undercarriage.
Specifications
- The Rotorvox C2A has a length of 5.5 m (18 ft).
- It has a wingspan of 8.4 m (28 ft).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
At least two prototypes were flown over five years of development, with the first flight around 2009. Deliveries began in October 2014.
Variants
No variants are listed in the source.
Where you'll see it
It is built by Rotorvox GGC GmbH and powered by a 73 kW Rotax 914 driving a three-blade propeller. The rotor is pre-rotated hydraulically.
Related aircraft
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