Boeing 767-300ER vs. Lockheed U-2
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Boeing 767-300ER |
versus |
Lockheed U-2 |
54.9 m |
180 ft 3 in |
length |
19.2 m |
63 ft 0 in |
15.85 m |
52 ft |
height |
4.8 m |
15 ft 9 in |
47.57 m |
156 ft 1 in |
wingspan |
32 m |
105 ft |
Two Pratt & Whitney PW4060 turbofan engines |
engines |
1 × General Electric F118-101 |
Up to 63,300 pounds of thrust each |
thrust per engine |
17,000 lbf (76 kN) |
Up to 126,600 pounds of thrust |
total thrust |
17,000 lbf (76 kN) |
186,880 kg |
412,000 lb |
MTOW |
18,144 kg |
40,000 lb |
11,070 km |
5,980 nm |
range |
6,090 nm |
11,278 km |
528 MPH |
850 km/h |
cruise speed |
475 mph |
764 km/h |
Typically 218 (3-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.