North American XB-28
1942
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North American XB-28

Envisaged originally as a high-altitude version of the B-25 Mitchell, the North American NA-63 (XB-28) emerged finally as an almost entirely different aircraft. With single vertical tail surfaces and a circular-section fuselage with a pressure cabin for the five-man crew, the XB-28 was powered by two 1491kW Pratt & Whitney R-2800 radials and bomb bay capacity was 1814kg. Dorsal, ventral and tail turrets, each containing two 12.7mm machine-guns, were remotely controlled from the cockpit; three similar forward-firing weapons were also fitted. Of three prototypes ordered in February 1940, the first flew in April 1942, the second was cancelled and the third, with a reconnaissance camera installation, crashed during the test programme. Although the XB-28 achieved a maximum speed of 599km/h at 7620m and could carry a 272kg bomb load for 3283km, production orders were not placed.

3-View 
North American XB-28A three-view drawing (700 x 1053)


Specification 
 WEIGHTS
    Take-off weight16226 kg35772 lb
    Empty weight11611 kg25598 lb
 DIMENSIONS
    Wingspan22.12 m72 ft 7 in
    Length17.20 m56 ft 5 in
    Wing area62.80 m2675.97 sq ft
 PERFORMANCE
    Cruise speed411 km/h255 mph
    Range3284 km2041 miles

North American XB-28

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