Cargo drone
based on UL/LSA 600kg fixed wing plane
Engine
| Manufacturer | Rotax |
| Model | 912 |
| Horsepower | 80 hp – 115 hp |
Weight
| Empty weight | 330 kg |
| Max. Take-off weight | 600 kg UL2 / LSA |
| Min. crew weight | 0 kg |
| Max. crew weight | 0 kg |
| Max. cargo weight | 200 kg |
Performance
| Takeoff | 150 m / 490 ft |
| Climb Rate | 5–7 m/s / 1200 ft/min |
| Max Operating Altitude | 5400 m / 18000 ft |
| Stall Speed with Flaps | 53 km/h / 29 kt |
| Max Cruise Speed | 250 km/h / 135 kt |
| Landing Groundroll | 150 m /490 ft |
Dimensions
| Lenght | 7,030 m |
| Height | 2,650 m |
| Wing span | 9,085 m |
| Wing area | 10,757 m2 |
| Horizontal tail width | 2,800 m |
| Horizontal tail area | 2,244 m2 |
| Vertical tail area | 1,116 m2 |
| Cabin width | 1,164 m |
SOPHISTICATED
AI UAV autopilot
• autonomous flight according 3D track in WGS84 coordinates
• autonomous flight according 2D track in WGS84 coordinates and altitude above the terrain
• auto start from defined airfield (could be grass runway)
• auto approach to the landing on specific runway (could be grass airfield)
• autonomous landing on specific runway (could be grass, but has to have at least 1.0 km)
Flight Data
• absolute plane position WGS84 | • relative plane position
• airspeed | • vertical speed
• altitudes: baro | satellite (above geoid) | radio/laser
• engine data: temperatures | pressures | rpm | fuel level
• compass bearing/heading
• calculated wind (speed, direction)
• side slip
• angle of attack
– sence & avoid system (prevents collisions with static or flying objects)
– telemetry with GCS (ground control station)
• flying telemetry
(realtime data down and mission plan changes up)
• video telemetry
• cargo telemetry