North American B-25 Mitchell  

 North American B-25 Mitchell

The B-25 was designed for the United States' Army Air Corps before the Second World War. The North American company had never designed a multi-engine bomber before. The original design had shoulder-mounted wings and a crew of three in a narrow fuselage. The USAAC then decided its new bomber would need a much larger payload, causing them to double the original specifications. North American designers dropped the wing to the aircraft's mid-section, and widened the fuselage so the pilot and co-pilot could sit side-by-side. They also improved the cockpit. The USAAC ordered 140 aircraft of the new design right off the drawing board. There were at least six major variants of the Mitchell, from the initial B-25A and B-25B, with two power-operated two-gun turrets, to the autopilot-equipped B-25C, and the B-25G with 75mm cannons for use on anti-shipping missions. In the end, the B-25 became the most widely used American medium bomber of World War Two.

 Specifications

Full Name

North American B-25B Mitchell

Type

Medium Bomber

Origin

USA

Manufacturer

North American

Wingspan

30.66 m

Length

16.13 m

Height

4.80 m

Weight

Empty: 9072 kg

Maximum Speed

483 km/h

Range

2172 km

Engine

2 x 1700hp Wright R-2600-9

Armament

1 x .3in machine gun, 4 x .5in machine guns

Crew

5

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