Boeing 777-200 vs. Lockheed U-2
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| Boeing 777-200 |
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 |
| General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 |
engines |
1 × General Electric F118-101 |
| Up to 94,000 pounds |
thrust per engine |
17,000 lbf (76 kN) |
| Up to 188,000 pounds |
total thrust |
17,000 lbf (76 kN) |
| 299,370 kg |
660,000 lb |
MTOW |
18,144 kg |
40,000 lb |
| 5,240 nm |
9,711 km |
range |
6,090 nm |
11,278 km |
| 560 mph |
901 km/h |
cruise speed |
475 mph |
764 km/h |
| 305 |
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.
