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Start | North American | B-25J Mitchell


General information


ManufacturerNorth American
ModelB-25J Mitchell
ModificationB-25J
CountryUSA
Years1943
TypeBomber
Main rotor diameter-
Tail rotor diameter-
Wingspan20.59 m
Length16.30 m
Height4.88 m
Wing area56.67 m2
Zero fuel weight-
Empty weight8840 kg
Maximum takeoff weight-
Normal takeoff weight15150 kg
Flight duration-
Engine2 Wright R-2600-29 Cyclone
Power2 x 1700 HP
Thrust-
Maximum speed444 km/h
Cruising speed370 km/h
Rate of climb-
Practical range2173 km
Service ceiling7470 m
Hovering ceiling-
Crew-
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