Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Lockheed Hudson Mk I Twin-Engine Multirole Aircraft.
2 x Wright Cyclone 9-cylinder air-cooled radial piston engines developing 1,100 horsepower each.
Propulsion
249 mph
400 kph | 216 kts
Max Speed
24,508 ft
7,470 m | 5 miles
Service Ceiling
1,957 miles
3,150 km | 1,701 nm
Operational Range
1,200 ft/min
366 m/min
Rate-of-Climb