Cruiser UAV

Cruiser UAV's philosphy

Designed as a high-performance unmanned aircraft, the Cruiser UAV platform balances robust lifting capacity with exceptional deployment flexibility. The structural design features a small footprint with a 3.2 m wingspan and supports up to a 20 kg maximum take-off mass (MTOW).

• Hybrid fixed-wing (CTOL & VTOL): Unlike traditional airframes, the Cruiser UAV simultaneously supports both CTOL and VTOL operations based strictly on the pilot's discretion.
• Optimized airframe aerodynamics: The tri-rotor tilt-rotor configuration of the Cruiser UAV ensures that only one rotor is not actively contributing to forward propulsion. This significantly reduces drag, directly increasing endurance.
• Maximized payload mass: The tri-rotor tilt-rotor configuration of the Cruiser UAV minimizes the overall weight of the propulsion system, allowing the integration of larger, heavier payloads by mass.

Procurment options

• Airframe only: Airframe ready for custom autopilot integration.
• With integrated avionics: Airframe and autopilot, configured and ready to fly.
• With integrated avionics and development package: Airframe and autopilot, configured and ready to fly with the addition of extensive documentation, SIL/HIL real-time simulators, and PX4 autopilot configuration files.

Documentation

AVIUM-TDS-0001 Technical Datasheet - Cruiser UAV.pdf