Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the North American B-25C Mitchell Twin-Engine Medium Bomber Aircraft.
2 x Wright Cyclone R-2600-19 air-cooled piston engines developing 1,700 horsepower each driving three-bladed propeller units.
Propulsion
272 mph
438 kph | 237 kts
Max Speed
24,196 ft
7,375 m | 5 miles
Service Ceiling
1,350 miles
2,173 km | 1,173 nm
Operational Range
1,666 ft/min
508 m/min
Rate-of-Climb