The Spear-1A is a large vertical-takeoff fixed-wing UAV with 180 kg maximum takeoff weight, 60 kg payload capacity, and up to 8 hours endurance for long-range missions.
Key Capabilities
- Vertical takeoff and landing (VTOL) capability
- 180 kg maximum takeoff weight with 60 kg payload
- 8-hour endurance at 40 kg payload, 4-hour at 60 kg
- 180 km/h maximum speed with 136.8 km/h cruise
- RTK dual-antenna GPS for precision positioning
- 55 L fuel capacity for extended range operations
Technical Specifications
| Fuselage length | 3,970 mm |
|---|---|
| Wingspan | 7,336 mm |
| Maximum takeoff weight | 180 kg |
| Maximum payload | 60 kg |
| Endurance time | 8 h @ 40 kg payload, 4 h @ 60 kg payload |
| Cruise speed | 136.8 km/h |
| Maximum speed | 180 km/h |
| Maximum fuel capacity | 55 L |
| Maximum wind resistance | 12 m/s |
| Takeoff and landing mode | Vertical takeoff and landing |
| Positioning system | RTK dual-antenna GPS |
Applications
Long-endurance surveillance, large-area mapping, cargo transport, border patrol, and extended-range reconnaissance missions.
Deployment note: Final configuration, operator training, airspace approval, and local regulatory compliance are required before deployment.
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