SL-400
The ATTICUS SL-400 is an industrial unmanned aircraft combining vertical take-off and landing capability with fixed-wing flight. Its twin-boom, compound-wing airframe and gasoline-plus-electric power configuration support material transport, aerial surveying, and environmental monitoring without requiring a conventional runway.
Operational Use Cases
Material Transport
Movement of supplies and equipment to remote locations.
Disaster Monitoring
Aerial observation to support assessment and response planning.
Environmental Monitoring
Observation of terrain, waterways, and changing environmental conditions.
Aerial Surveying
Survey and mapping missions with appropriately configured payloads.
Specifications
| Parameter | Specification |
|---|---|
| Maximum Takeoff Weight | 370 kg |
| Maximum Payload | 100 kg (stated) |
| Maximum Range | 2,000 km (stated) |
| Airframe Length | 5,600 mm |
| Airframe Width | 8,300 mm |
| Airframe Height | 1,500 mm |
| Maximum Ceiling | 5,200 m |
| Maximum Flight Time | 8 hours (stated) |
| Maximum Flight Speed | 310 km/h (stated) |
| Power Configuration | Gasoline + electric |
| Airframe Configuration | Twin-boom, compound-wing VTOL |
Specifications are supplier-stated and have not been independently verified. Maximum range, payload, endurance, and speed are individual limits and are not assumed to occur simultaneously. Propulsion and charging arrangements require confirmation for the offered configuration.
Ready to Deploy the F8?
Contact our team to discuss configuration, integration, and support options for your specific operational requirements.