More than 17 hours of flight in horizontal mode and more than 8 in vertical takeoff. Both at maximum 4,500 meters AGL ISA

MTOW of 38 kg in HTOL, 42 kg in VTOL configuration

14 kg (31 lb) in HTOL mode or 5 kg (11 lb) in payload VTOL mode, 100% convertible between fuel, batteries, or payload. No ballasts to adjust the center of gravity

Redundancy in critical navigation, power, electrical, wiring, servo actuators, and autopilot systems

A maximum speed of 110 km/h, and 90 km/h cruising speed.

Below cloud level stealth

• 100% automatic operation, minimize human error

• Landing abort when it loses track alignment automatically executes a new attempt

• Smart return to base, following the same outbound flight path, avoiding detection, obstacles, and restricted flight zones

• Automatic return to base on communication failure, low fuel, or GPS failure

• Automated speed management to increase flight time (default) or maximize distance traveled

• Computer-assisted manual flight mode option

• Constant monitoring of sensors in engines with automated fault response management

• Automatic runway selection depending on runway wind conditions

• In vertical takeoff and landing, it automatically maintains vertical over the point despite the wind, avoiding obstacles or an off-target landing

• In conventional take-off and landing, it maintains the course automatically despite the wind, avoiding obstacles, to complete a safe landing operation