Airbus A321-200 vs. Douglas DC-8-61
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Airbus A321-200 |
versus |
Douglas DC-8-61 |
44.51 m |
146 ft 0 in |
length |
57.0 m |
187 ft 0 in |
11.76 m |
38 ft 7 in |
height |
13.1 m |
43 ft |
35.8 m |
117 ft 5 in |
wingspan |
45.24 m |
148 ft 5 in |
2 GE CFM56-5B3 |
engines |
4x P&W JT3D-3B Turbofan |
31,600 lbs |
thrust per engine |
18,000 pound-force |
63,200 lbs |
total thrust |
72,000 pound-force |
89,000 kg |
196,200 lb |
MTOW |
147,400 kg |
325,000 lb |
4,000 nmi |
7,408 km |
range |
3,200 nm |
5,926 km |
871 km/h |
541 mph |
cruise speed |
483 knots |
282 mph |
185 to 220 |
capacity |
180 to 220 passengers in a mixed-class seating |
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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.