Complaint
| Diameter of main rotor: | 3220mm |
| overall length: | 3680mm (from the front to the rear of the main rotor) |
| Maximum width: | Conventional landing gear: 700mm; High landing gear: 800mm |
| Maximum height: | Conventional landing gear: 1100mm; High landing gear: 1300mm |
| Engine type | Piston engine |
| Cylinder | Double cylinder, horizontally opposed |
| Fuel type | Motor gasoline 92-95# |
| Oil ratio | 2T FD grade fully synthetic engine oil; 50:1 |
| displacement | 250cc |
| Cooling mode | Liquid cooling |
| Starting mode | Airborne electric starting (manual, remote control optional) |
| Airborne power supply | Lithium iron phosphate battery (Li Fe) 4500mah+2500mah |
| Voltage | 14V |
| Airborne generator power | 14V 145W or 235W |
| Body weight | 57kg (excluding fuel) |
| Standard takeoff weight (standard atmospheric pressure) | 85kg |
| Maximum takeoff weight (standard atmospheric pressure) | 100KG |
| Maximum payload (standard atmospheric pressure) | 35kg |
| Cruise speed | 0-90Km/h |
| Max climb rate | 6m/s |
| Maximum flight speed | 70Km/h |
| Maximum endurance | Main oil tank 90 minutes Add auxiliary oil tank for 300 minutes |
| Take-off and landing mode | Manual takeoff and landing or fully autonomous takeoff and landing |
| Navigation mode | RTK base station, GPS+Beidou |
| Working distance | 1-20km (depending on the customer's use) |
| Maximum wind resistance | Maximum force 6 wind (wind speed 10.8m/s) in autonomous fixed point hovering state |
| Operating temperature range | Min. - 25 ºC Max.+45 ºC |
| Operating humidity range | 40%-70% |
| Maximum flight altitude | 3000m above sea level (13kg load) |
