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The North American B-25 Mitchell owed its beginnings to the Army's quest for a medium bomber. The B-18 "Bolo" was designed and built by Douglas Aircraft in 1937 and North American responded to this by designing and building the larger and more powerful B-21 "Dragon" that same year. Both of these aircraft were twin engine "tail dragger" types. Unsatisfied with performance only marginally better than single engine aircraft, the US Army Air Corps issued Proposal Circular #38-385 which was sent to all major aircraft manufacturers in March 1938. It contained the requirements for an "Aircraft - Bombardment Type - Medium". This would fill a gap in the bombing aircraft types between the light bomber and four engine heavy bomber. A total of 5 manufacturers submitted designs (North American, Douglas, Martin, Stearman and Bell) and all but one built prototypes. North American submitted their "Design NA-40" to the USAAC and shortly afterward built the NA-40B prototype. It was a sleek looking twin engine, twin tail machine with tricycle landing gear, not unlike the B-25 and fairly bristling with .30 Cal. (7.62 mm) machine guns. Unfortunately, while undergoing simulated "engine out" tests, the pilot lost control and the aircraft crashed. The pilot and crew escaped with minor injuries but the NA-40B was destroyed by fire and North American was disqualified, though the Army deemed the accident caused by pilot error and not by anything inherent in the design of the NA-40B. That left only 3 prototypes competing and shortly, one of these also crashed and burned (the Douglas 7B) and was disqualified, leaving less than half the original bidders still competing. The USAAC ruled no contest, and though Glenn Martin raised vigorous objections, new bids were ordered to be submitted in April, 1939.

The result from North American was a dramatically updated NA-40, redesignated the NA-62. The design was much more streamlined with the rear of the "greenhouse" canopy neatly faired into the fuselage (instead of the "upside down bathtub" of the NA-40), forming a straight line from the top of the windshield to the tail assembly. On August 10, the design was accepted by the USAAC as the B-25 and
ordered into production straight off the drawing board, something not often done with new aircraft. The B-25 was fitted with two turbo supercharged Wright R-2600 Cyclone radial engines and though the dash numbers changed and modifications were made to it, the supercharged R-2600 Cyclone was standard through the final production model which was the B-25J.

North American B-25J "Mitchell" Medium Bomber
Wing span: Wing Span: 67 ft 7 in (20.59 m)
Length: Length: 51 ft (15.55 m)
Height: Height: 16 ft 4 in (4.98 m)
Wing Area: 610 sq ft (56.67 mē)
Empty: 19,530 lb (8,858 kg)
Gross: 26,122 lb (11,848 kg)
Maximum T/O: 35,000 lb. (15,876 kg)
Maximum Speed: 285 mph (458 kph) at 15,000 ft (4,572 m)
Cruising Speed: 230 mph (370 kph)
Service Ceiling: 24,200 ft (7,376 m)
Normal Range: 1,350 miles (2,172 km) with
3,000 lbs (1,360 kg) of bombs
Maximum Range: 2,200 miles (3,540 km) with ferry tanks
Two R-2600-29 Wright "Cyclone" 14 cylinder, air cooled radial
engines developing 1,700 hp (1,268 kW) each for T/O
Eighteen .50 cal (12.7 mm) M-2 Colt-Browning machine guns.
Up to 3,200 lbs (1,451 kg) of bombs


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Digger History:  an unofficial history of the Australian & New Zealand Armed Forces