Specifications
| Parameter | Details |
| Aircraft type | Flying wing |
| Wingspan | 1.7 m |
| Wing area | 0.667 m² |
| All-up weight (AUW) | 3.5 kg |
| Design payload capacity | 1.2 kg (platform design target) |
| Documented/operational
payload |
800 g |
| Maximum speed | 25–27 m/s |
| Cruise speed | 12 m/s |
| Range | 5 km |
| Battery | 5200 mAh, 4S LiPo |
| Endurance | 5–8 minutes |
| Stall speed | 8.5 m/s |
| Avionics | GPS: Yes; Autopilot: Yes |
| FPV system | Yes |
| Current focus | Airframe validation and safe avionics integration |
Description
A compact loitering-munition platform engineered for precision terminal strikes. The flying-wing airframe prioritizes low weight and aerodynamic efficiency to maximize maneuverability and accuracy during terminal approach. The system integrates GPS-guided autonomy, an onboard autopilot and an FPV link for operator oversight, enabling reliable navigation to and engagement of designated targets within a ~5 km standoff. Current development work concentrates on validating the airframe structure and integrating avionics with redundant safety checks to ensure dependable operation during autonomous and semi-autonomous missions.