BGKT-3000 (High-Altitude Version)
| BGKT-3000 Performance Specifications | ||
|---|---|---|
| Item | Specification | Unit / Note |
| Platform | BGKT-3000 tandem twin-rotor unmanned helicopter platform | — |
| Max take-off weight | 380 | kg |
| Max payload | 150 | kg |
| Endurance | 4 | hours (max endurance 7 h) |
| Max operating altitude | 3,500 | m AMSL |
| Max speed | 145 | km/h (cruise 120 km/h) |
| Wind resistance | ≤ 7 | Beaufort scale |
| Engine | C100 | aero engine |
| Rotor diameter | 3,400 | mm |
| Dimensions (L×W×H) | 3,000 × 1,000 × 1,300 | mm |
| Flight-control modes | Remote control, command guidance, autonomous navigation, automatic return-to-home, failsafe protection |
— |
| Flight modes | Point hover; constant-speed / constant-altitude cruise; coordinated turns; sloping climb / spiral climb; stabilized take-off and landing; fully automatic take-off and landing |
— |
| Navigation system | GPS / BeiDou / Galileo with RTK differential GPS | — |
| Positioning accuracy | < 10 | cm |
| Control radius | Line-of-sight 150 | km (expandable to 200 km) |
| Ground control station | Windows-based GCS with electronic map, virtual instruments, integrated display, command panel, route planning, status monitoring and alarm functions |
— |
| Mission payloads | Supports integration of EO/IR gimbal, seawater sampler, spraying system, payload dropper/launcher, firefighting bombs, rescue pods, etc. |
— |
