Products/Unmanned Aerial Systems
VTOL PLATFORMAir & Space

SL-400

Compound-Wing Vertical Take-Off and Landing UAV

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.

2,000 kmMax Range
100 kgMax Payload
8 hrsEndurance
310 km/hMax Speed
ATTICUS SL-400 compound-wing VTOL UAV — overhead three-quarter view
Applications
01

Material Transport

Movement of supplies and equipment to remote locations.

02

Disaster Monitoring

Aerial observation to support assessment and response planning.

03

Environmental Monitoring

Observation of terrain, waterways, and changing environmental conditions.

04

Aerial Surveying

Survey and mapping missions with appropriately configured payloads.

Technical Specifications
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. No independently verified resistance-to-interference claim is made.

Request Platform Information

Contact the ATTICUS Air & Space division for procurement inquiries, integration specifications, and capability briefings on the SL-400 platform.