NORTH AMERICAN B-25 MITCHELL

 

Origin:

United States of America

Type:

Twin-engine light-to-medium bomber

Engine:

(B-25J) Two 1,268 kw (1,700 hp) Wright Cyclone R-2600-29 fourteen-cylinder two-row radial air-cooled engines

Specifications:

  • Wingspan: 20.42 m (67 ft 6 in)
  • Length: 16.12 m (52 ft 11 in)
  • Height: 4.8 m (15 ft 9 in)
  • Wing area: 56.66 m² (610 sq ft)
  • Max speed at 4,572 m (15,000 ft): 442 km/h (275 mph)
  • Cruising speed: 322 km/h (200 mph)
  • Initial rate of climb: 338 m/min (1,110 ft/min)
  • Service ceiling: 7,620 m (25,000 ft)
  • Range with 1,451 kg (3,200 lb) bomb load and 4,037 litres (811 Imp gals) of fuel at max cruising speed: 2,052 km (1,275 miles)
  • Empty weight: 15,196 kg (33,500 lb)
  • Loaded weight: 18,960 kg (41,800 lb)

Photo source: Wikipedia

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