Airbus A350-800 vs. Lockheed U-2
... or view the full comparison list
here.
Airbus A350-800 |
versus |
Lockheed U-2 |
60.54 m |
198 ft 7 in |
length |
19.2 m |
63 ft 0 in |
17.05 m |
55 ft 11 in |
height |
4.8 m |
15 ft 9 in |
64.7 m |
212 ft 5 in |
wingspan |
32 m |
105 ft |
2 Turbofans (wing mounted) |
engines |
1 × General Electric F118-101 |
75,760 lb |
thrust per engine |
17,000 lbf (76 kN) |
151,520 lb |
total thrust |
17,000 lbf (76 kN) |
283,000 kg |
623,900 lb |
MTOW |
18,144 kg |
40,000 lb |
11,708 km |
6,319 nm |
range |
6,090 nm |
11,278 km |
552 mph |
888 km/h |
cruise speed |
475 mph |
764 km/h |
Typically carries 300 to 350 passengers |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.