Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the HAI Pegasus Mk II Reconnaissance Unmanned Air System (UAS).
1 x Conventional engine at rear of fuselage driving two-bladed propeller unit in pusher arrangement.
Propulsion
99 mph
160 kph | 86 kts
Max Speed
1,243 miles
2,000 km | 1,080 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).