Description
- New Text Heavy-Lift Hybrid Multi-Rotor UAV
Parameters
| General | |
|---|---|
| New Aircraft Type | Multi-rotor (6 rotors) |
| Power System | Range-extended hybrid (gasoline) |
| Engine Type | Four-stroke |
| Engine Displacement | 850 cc × 2 |
| Dimensions | |
| Wheelbase | 3850 mm |
| Unfolded Size | 3505 × 4021 × 1480 mm |
| Transport Size | 2110 × 1910 × 1480 mm |
| Weight & Payload | |
| Empty Weight | ≤ 260 kg |
| Max Takeoff Weight | ≥ 500 kg |
| Max Payload | ≥ 200 kg |
| Performance | |
| Endurance (Full Load) | ≥ 60 min |
| Endurance (No Load) | ≥ 90 min |
| Max Speed | ≥ 15 m/s |
| Climb Speed | ≥ 3 m/s |
| Descent Speed | ≥ 2 m/s |
| Maximum Range | ≥ 50 km |
| Control & Accuracy | |
| Hover Accuracy (GNSS) | H ±1 m / V ±1.5 m |
| Hover Accuracy (RTK) | H ±0.5 m / V ±0.5 m |
| Communication Distance | ≥ 5 km (customizable) |
| Power & Fuel | |
| Total Power | ≥ 80 kW |
| Fuel Type | 92# or higher gasoline |
| Fuel Tank | 50 L |
| Environment | |
| Wind Resistance | ≥ Level 5 |
| Rainproof | Light rain operation |
| Operating Temperature | -20°C ~ +50°C |
