CEOS project| Take-off weight: | 25 kgs |
| Dimension: | Distance between motors: 1150 mm Height: 800mm |
| Power: | LiPo 12S 44 Ah (2x2 LiPo 6S 22 Ah in series) |
| Maximum thrust: | 70 kgs |
| Take-off maximum weight: | 30 kgs |
| Maximum thrust versus weight ratio: | 2.8 at 0 meter altitude / 2.1 at 2500 meters altitude |
| Range at 25km/h: | 5.6 kms (in 12 minutes) |
| Maximum speed: | 75 kms/h |
| Hovering power: | 4.2 kW |
| Maximum power: | 17.8 kW |
| Emergency systems: | Parachute + engines cut |
| Drone impact energy with emergency systems: | 250 J |
| Transportation: | Foldable drone on the length Transportation volume: 1150 x 250 x 400 mm |
