Concorde vs. North American F-100 Super Sabre
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here.
| Concorde |
versus |
North American F-100 Super Sabre |
| 61.66 m |
202 ft 4 in |
length |
16.46 m |
54 ft 2 in |
| 11.4 m |
37 ft 5 in |
height |
4.93 m |
16 ft 2 in |
| 25.56 m |
83 ft 1 |
wingspan |
11.84 m |
38 ft 1 |
| 4 Rolls Royce/Snecma Olympus 593 turbo jet engines |
engines |
1 Pratt & Whitney J57-P-21A |
| 18.7 tons (180 kN) |
thrust per engine |
16,000 lb. thrust in afterburner |
| 74.8 tons (720 kN) |
total thrust |
16,000 lb. (afterburner) |
| 185,000 kg |
408,000 lb |
MTOW |
17,609 kg |
38,800 lb |
| 6,580 km |
3,554 nm |
range |
2,673 km |
1,444 nm |
| Mach 2.04 |
2,179 km/h |
cruise speed |
587 mph |
945 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.
