Concorde vs. Lockheed U-2
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Concorde |
versus |
Lockheed U-2 |
61.66 m |
202 ft 4 in |
length |
19.2 m |
63 ft 0 in |
11.4 m |
37 ft 5 in |
height |
4.8 m |
15 ft 9 in |
25.56 m |
83 ft 1 |
wingspan |
32 m |
105 ft |
4 Rolls Royce/Snecma Olympus 593 turbo jet engines |
engines |
1 × General Electric F118-101 |
18.7 tons (180 kN) |
thrust per engine |
17,000 lbf (76 kN) |
74.8 tons (720 kN) |
total thrust |
17,000 lbf (76 kN) |
185,000 kg |
408,000 lb |
MTOW |
18,144 kg |
40,000 lb |
6,580 km |
3,554 nm |
range |
6,090 nm |
11,278 km |
Mach 2.04 |
2,179 km/h |
cruise speed |
475 mph |
764 km/h |
92–120 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.