Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the LSU-02 ISR Unmanned Aerial Vehicle (UAV) / Drone.
1 x Conventional engine driving two-bladed propeller at rear of fuselage in pusher arrangement.
Propulsion
62 mph
100 kph | 54 kts
Max Speed
9,843 ft
3,000 m | 2 miles
Service Ceiling
280 miles
450 km | 243 nm
Operational Range