North American XB-21
1937
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North American XB-21

Similar in appearance to the Douglas B-18 Bolo, but intended to achieve significantly improved performance, the North American NA-21 bomber was developed at the company's Inglewood, California plant during 1935-3, the prototype being completed in March 1937. Powered by two 895kW Pratt & Whitney R-218.0 Twin Hornet engines with F-10 turbo-superchargers, the XB-21 carried a six-man crew and armament comprised single 7.62mm machine-guns in nose and dorsal turrets, plus a similar weapon in each of the ventral and two waist positions. Short-range bomb load was 4536kg, reducing to 998kg over 3058km.

Only the prototype was built.

3-View 
North American XB-21A three-view drawing (574 x 745)


Specification 
 WEIGHTS
    Take-off weight18144 kg40001 lb
 DIMENSIONS
    Wingspan28.96 m95 ft 0 in
 PERFORMANCE
    Max. speed354 km/h220 mph

North American XB-21

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