Bombardier CRJ1000 vs. North American B-25 Mitchell
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Bombardier CRJ1000 |
versus |
North American B-25 Mitchell |
39.1 m |
128 ft 5 in |
length |
16.15 m |
53 ft 0 in |
7.5 m |
24 ft 7 in |
height |
5 m |
16 ft 4 in |
26.2 m |
86 ft |
wingspan |
20.58 m |
67 ft 6 in |
2 GE CF34-8C5A1 turbofans |
engines |
2 x Wright R-2600-92 Twin Cyclone |
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve |
thrust per engine |
1,700 horsepower |
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
total thrust |
3,400 horsepower |
41,640 kg |
91,800 lb |
MTOW |
7,484 kg |
16,500 lb |
3,004 km |
1,623 nm |
range |
1,350 mi |
1,175 nm |
515 mph |
829 km/h |
cruise speed |
233 MPH |
375 km/h |
100 (common) |
capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.