Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Chengdu Wing Loong III Unmanned Combat Air System (UCAS).
1 x Conventional turboprop engine of unknown make, model, and output power driving five-bladed propeller unit at the rear of the fuselage in pusher arrangement.
Propulsion
249 mph
400 kph | 216 kts
Max Speed
162 mph
260 kph | 140 kts
Cruise Speed
32,808 ft
10,000 m | 6 miles
Service Ceiling
4,350 miles
7,000 km | 3,780 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).