| dual-rotor UAV | Max take off weight | 650Kg |
| Standard payload | ≮260KG (below 3000 meter altitude) ≮200KG (below 3000 meter altitude) | |
| Endurance | 2-4H | |
| Max height | 6500 meter altitude | |
| Max speed | 160Km/h | |
| Aviation engine | 141HP，water cooler | |
| Rotor diameter | 480 cm | |
| Wind class | ≥7 | |
| Size | 400/130/190 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 | ≥100KM | |
| 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. |