Airbus A321-200 vs. Lockheed U-2
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Airbus A321-200 |
versus |
Lockheed U-2 |
44.51 m |
146 ft 0 in |
length |
19.2 m |
63 ft 0 in |
11.76 m |
38 ft 7 in |
height |
4.8 m |
15 ft 9 in |
35.8 m |
117 ft 5 in |
wingspan |
32 m |
105 ft |
2 GE CFM56-5B3 |
engines |
1 × General Electric F118-101 |
31,600 lbs |
thrust per engine |
17,000 lbf (76 kN) |
63,200 lbs |
total thrust |
17,000 lbf (76 kN) |
89,000 kg |
196,200 lb |
MTOW |
18,144 kg |
40,000 lb |
4,000 nmi |
7,408 km |
range |
6,090 nm |
11,278 km |
871 km/h |
541 mph |
cruise speed |
475 mph |
764 km/h |
185 to 220 |
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.