Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the UKRSPEC Systems PD-1 ISR Unmanned Aerial System (UAS) / Drone.
1 x 61cc 2-cylinder, 4-stroke conventionally-fueled engine driving two-bladed propeller unit at rear of fuselage in pusher configuration.
Propulsion
47 mph
75 kph | 40 kts
Max Speed
40 mph
65 kph | 35 kts
Cruise Speed
9,843 ft
3,000 m | 2 miles
Service Ceiling
342 miles
550 km | 297 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).