Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the NCSIST Cardinal II ISR Small Unmanned Aircraft System (SUAS).
1 x Engine seated at the front of the fuselage driving a two-bladed propeller unit in tractor arrangement.
Propulsion
34 mph
55 kph | 30 kts
Max Speed
1,969 ft
600 m | 0 miles
Service Ceiling
31 miles
50 km | 27 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).