| dual-rotor UAV | Max take off weight | 300kgs |
| Standard payload | 140kgs (below 3000 meter altitude ) | |
| Endurance | 3-4H | |
| Max height | 3500 meter altitude | |
| Max speed | 120Km/h | |
| Aviation engine | 65HP，water cooler | |
| Rotor diameter | 340cm | |
| Wind class | ≥6 | |
| Size | 300/100/130 CM （L/W/H） | |
| OH Flight controller | Control modes | Remote control, instruction navigation, automatic navigation, automatic return, out of control protection |
| Flight modes | Fixed -point hover, fixed speed/fixed -high cruise, coordinated turning, oblique climb/hovering climbing, increased stability, take -off/landing, automatic take -off/landing | |
| GPS/Beidong/Glonass | RTK & GPS | |
| Accuracy | < 10CM | |
| Control range | ≥60KM | |
| Ground station | Windows ，e-map、virtual instrument、e-display、command panel、route setting 、Status monitoring and alarm function | |
| Applications | Support integrated optoelectronic pods, seawater samplers, shouts, throwers, etc. |