North American B-25 Mitchell vs. Douglas DC-8

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North American B-25 Mitchell versus Douglas DC-8
16.15 m 53 ft 0 in length 57.10 m 187 ft 4 in
5 m 16 ft 4 in height 16.84 m 55 ft 3 in
20.58 m 67 ft 6 in wingspan 45.24 m 148 ft 5 in
2 x Wright R-2600-92 Twin Cyclone engines 4 x Pratt & Whitney JT3D turbofan engines
1,700 horsepower thrust per engine Approximately 17,000 lbf per engine
3,400 horsepower total thrust Approximately 68,000 lbf total
7,484 kg 16,500 lb MTOW 158,760 kg 350,000 lb
1,350 mi 1,175 nm range 11,918 km 6,437 nm
233 MPH 375 km/h cruise speed 900 km/h 559 mph
capacity Up to 259 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.