Fuselage (L×W×H) | 2895×616×1150mm | Maximum flight speed | 120km/h |
Total length of fuselage (including propeller) | 3765mm | Maximum endurance | 8 hours |
| Diameter of main propeller | 3330mm | Maximum operating radius | 100km |
| Tail rotor diameter | 620mm | Practical cruising altitude | 3000m |
| Gross takeoff weight | 110kg (fuselage + load) | Maximum lift | 4000m |
| Self-weight | 65kg | Operating Temperature | -20-40°C |
| Maximum task load | 50kg | Wind resistance class | 6 |
| Engine Brand | Italy Raytheon | Transmission | Gear+Belt |
| Engine Displacement | 250cc | Main Fuel Tank | 12L |
Stroke | Two-stroke | Sub-tank (optional) | 9L*2 (on request) |
| Fuel consumption/hour | 6L/h | Engine operating voltage | 12V |
| Fuel grade | 98# gasoline | Avionics operating voltage | 24V |
| Engine oil | Two-stroke special oil | On-board generator | 12V/80W (for engine) 24V/800W (for avionics) |
Fuel/Oil Mixing ratio | 40:1 | Engine Starting Battery | 4700mAh |
| Starting method | Electric start | Battery pack for avionics | 5300mAh×2 (parallel connection) |
| Cooling method | Water-cooled + electronic fan | Control and Image Transmission distance (kilometers | 30、50、100（Optional on demand) |
| Control mode | Manual, semi-automatic, fully autonomous | Visual head | Single-light, double-light, triple-light (optional on request) |