Boeing 747-8I vs. Lockheed U-2
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Boeing 747-8I |
versus |
Lockheed U-2 |
76.25 m |
250 ft 2 in |
length |
19.2 m |
63 ft 0 in |
19.35 m |
63 ft 6 in |
height |
4.8 m |
15 ft 9 in |
68.45 m |
224 ft 7 in |
wingspan |
32 m |
105 ft |
4x General Electric GEnx 2B67 Turbofan |
engines |
1 × General Electric F118-101 |
66,500 pounds |
thrust per engine |
17,000 lbf (76 kN) |
266,000 pounds |
total thrust |
17,000 lbf (76 kN) |
443,613 kg |
977,500 lb |
MTOW |
18,144 kg |
40,000 lb |
8,000 nm |
14,816 km |
range |
6,090 nm |
11,278 km |
Mach 0.86 |
1,062 km/h |
cruise speed |
475 mph |
764 km/h |
467 passengers (three-class configuration) |
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.