Airbus A320neo vs. Lockheed U-2
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Airbus A320neo |
versus |
Lockheed U-2 |
37.57 m |
123 ft 3 in |
length |
19.2 m |
63 ft 0 in |
11.76 m |
38 ft 7 in |
height |
4.8 m |
15 ft 9 in |
35.8 m |
117 ft 5 in |
wingspan |
32 m |
105 ft |
2 x PW 1100G or 2 x CFM LEAP-1A |
engines |
1 × General Electric F118-101 |
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) |
thrust per engine |
17,000 lbf (76 kN) |
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) |
total thrust |
17,000 lbf (76 kN) |
79,000 kg |
174,200 lb |
MTOW |
18,144 kg |
40,000 lb |
6,300 km |
3,403 nm |
range |
6,090 nm |
11,278 km |
M0.82 |
101,3 km/h |
cruise speed |
475 mph |
764 km/h |
150-180 |
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.