Boeing 757-200 vs. Lockheed U-2
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Boeing 757-200 |
versus |
Lockheed U-2 |
47.3 m |
155 ft 2 in |
length |
19.2 m |
63 ft 0 in |
13.56 m |
44 ft 6 in |
height |
4.8 m |
15 ft 9 in |
38.1 m |
125 ft |
wingspan |
32 m |
105 ft |
Rolls-Royce RB211 or Pratt & Whitney PW2000 |
engines |
1 × General Electric F118-101 |
36,600–43,500 lbf (163–193 kN) |
thrust per engine |
17,000 lbf (76 kN) |
77,000 to 80,000 pounds |
total thrust |
17,000 lbf (76 kN) |
115,666 kg |
255,000 lb |
MTOW |
18,144 kg |
40,000 lb |
6,300 km |
3,400 nm |
range |
6,090 nm |
11,278 km |
876 km/h |
544 mph |
cruise speed |
475 mph |
764 km/h |
200 passengers |
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.