Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the ZHZ TD220 Unmanned Helicopter System (UHS).
1 x Gasoline- / kerosene-fueled conventional engine developing 65 horsepower driving 2 x Two-bladed main rotor units in coaxial arrangement atop the fuselage.
Propulsion
75 mph
120 kph | 65 kts
Max Speed
13,123 ft
4,000 m | 2 miles
Service Ceiling
342 miles
550 km | 297 nm
Operational Range