Composite single-seat plastic aircraft with a small wingspan. Designed with a unique aerodynamic scheme of a canard with an annular wing. This scheme allows takeoff and landing in a crosswind without stalling into a spin, as well as creating a rigid and lightweight apparatus. Aerodynamics allows flights at critical angles of attack.
Intended for:
| Category | Parameter | Value |
|---|---|---|
| General | Crew | 1 |
| Powerplant | Engine Power | 33 hp |
| Fuel Tank Capacity | 20 l | |
| Flight Performance | Cruising Speed | 180 km/h |
| Flight Range | 540 km | |
| Rate of Climb | up to 7 m/s | |
| Maximum Flight Altitude | 3,700 m | |
| Take-off & Landing | Take-off Run | 120 m |
| Landing Roll | up to 100 m | |
| Dimensions | Length | 4.6 m |
| Height | 1.9 m | |
| Wingspan | 2.8 m | |
| Weights | Empty Weight | 114 kg |
| Max Take-off Weight | 270 kg |
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