Boeing 777-200LR Worldliner vs. Lockheed U-2
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Boeing 777-200LR Worldliner |
versus |
Lockheed U-2 |
63.7 m |
209 ft 1 in |
length |
19.2 m |
63 ft 0 in |
18.6 m |
61 ft |
height |
4.8 m |
15 ft 9 in |
64.8 m |
212 ft 7 in |
wingspan |
32 m |
105 ft |
2 x GE90-115B |
engines |
1 × General Electric F118-101 |
115,300 lbf |
thrust per engine |
17,000 lbf (76 kN) |
230,600 lbf |
total thrust |
17,000 lbf (76 kN) |
347,500 kg |
766,100 lb |
MTOW |
18,144 kg |
40,000 lb |
15,843 km |
8,555 nmi |
range |
6,090 nm |
11,278 km |
950 km/h |
590 mph |
cruise speed |
475 mph |
764 km/h |
317 (2-class) |
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.