BGKT-5000 (Heavy Oil Type)Longitudinal-type Twin-rotor Unmanned Helicopter Platform
BGKT-5000 tandem twin-rotor unmanned helicopter platform
| Content | Parameters |
| Max take-off weight | 700 kg (including fuel) |
| Max payload | 300 kg (flat deck) |
| Endurance | 2–4 hours (max endurance 10 hours) |
| Max operating altitude | 7,000 m AMSL |
| Max speed | 160 km/h |
| Cruise speed | 140 km/h |
| Wind resistance | ≤ Beaufort scale 7 |
| Engine | 175 HP water-cooled aero engine |
| Rotor diameter | 4,800 mm |
| Dimensions | – Deployed: 7,500 × 4,200 × 2,250 mm
– Folded: 4,230 × 1,300 × 2,250 mm |
| Flight-control modes | remote control, command guidance, autonomous navigation, automatic return-to-home |
| 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 | ≥ 100 km, expandable up to 200 km |
| Ground control station | Windows-based; supports electronic map, virtual instruments, integrated situation display, command panel, route planning, status monitoring and alarm functions |
| Mission payloads | supports integration of EO/IR gimbal, seawater sampler, sprayer, payload dropper/launcher, firefighting bombs, rescue kits, etc. |
