Boeing 767-200ER vs. Lockheed U-2
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Boeing 767-200ER |
versus |
Lockheed U-2 |
48.5 m |
159 ft 2 in |
length |
19.2 m |
63 ft 0 in |
16.1 m |
52 ft 10 in |
height |
4.8 m |
15 ft 9 in |
47.8 m |
156 ft 9 in |
wingspan |
32 m |
105 ft |
2 x GE CF6-80C2B4F |
engines |
1 × General Electric F118-101 |
62,020 lbs |
thrust per engine |
17,000 lbf (76 kN) |
124,040 lbs |
total thrust |
17,000 lbf (76 kN) |
164,200 kg |
362,000 lb |
MTOW |
18,144 kg |
40,000 lb |
12,200 km |
6,587 nmi |
range |
6,090 nm |
11,278 km |
850 km/hour |
528 mph |
cruise speed |
475 mph |
764 km/h |
249 |
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.