Boeing 777-300ER vs. Lockheed U-2
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| Boeing 777-300ER |
versus |
Lockheed U-2 |
| 73.9 m |
242 ft 4 in |
length |
19.2 m |
63 ft 0 in |
| 18.5 m |
60 ft 8 in |
height |
4.8 m |
15 ft 9 in |
| 64.8 m |
212 ft 7 in |
wingspan |
32 m |
105 ft |
| GE90-115BL |
engines |
1 × General Electric F118-101 |
| 115,300 lbf (513 kN) |
thrust per engine |
17,000 lbf (76 kN) |
| 230,600 lbf (1026 kN) |
total thrust |
17,000 lbf (76 kN) |
| 351,534 kg |
775,000 lb |
MTOW |
18,144 kg |
40,000 lb |
| 13,649 km |
7,370 nmi |
range |
6,090 nm |
11,278 km |
| 510 knots |
945 km/h |
cruise speed |
475 mph |
764 km/h |
| 396 passengers (2-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.
