Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the NCSIST Albatross I ISR Unmanned Aircraft System (UAS).
1 x Conventional engine fitted to rear of fuselage driving two-bladed propeller unit in pusher arrangement.
Propulsion
93 mph
150 kph | 81 kts
Max Speed
13,123 ft
4,000 m | 2 miles
Service Ceiling
1,336 miles
2,150 km | 1,161 nm
Operational Range