| Basic Specifications | |
|---|---|
|
Wing span |
26.3ft |
|
MTOM |
Up to 850kg |
|
Fuel tank capacity |
190L + extra fuel tank of 200 L (Auto Motive Gasoline) |
|
Takeoff distance |
Ground roll: 950 ft. |
|
Landing distance |
Ground roll: 680 ft. |
|
Ballistic parachute |
Yes (optional) |
|
Engine |
4 cylinder 1.5 130HP |
|
Propeller |
2 or 3 blades |
|
Baseline certification |
Structure and sustems according to ASTM F2245 Airframe;
Basically composites |
|
Payload configuration |
TBD: Under the fuselage for gimbal - Hard-points under the wings (Estimated Payload from 250kg up to 300kg) |
| Performances | |
|---|---|
|
Max altitute |
22,000 ft |
|
Typical operating altitudes |
12,000 - 18,000 ft |
|
Speed in transfer to/from work area |
112 kt to 162 kt |
|
Loitering speed |
75 kt to 90 kt |
|
Endurance at transfer speeds |
15 to 18 hours |
