Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the LSU-03 ISR Unmanned Aerial Vehicle (UAV) / Drone.
1 x Conventional piston engine at rear of fuselage driving three-bladed propeller unit in pusher arrangement.
Propulsion
93 mph
150 kph | 81 kts
Max Speed
62 mph
100 kph | 54 kts
Cruise Speed
11,483 ft
3,500 m | 2 miles
Service Ceiling
373 miles
600 km | 324 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).