Concorde vs. McDonnell Douglas F-4 Phantom II
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Concorde |
versus |
McDonnell Douglas F-4 Phantom II |
61.66 m |
202 ft 4 in |
length |
19.2 m |
63 ft 0 in |
11.4 m |
37 ft 5 in |
height |
5.03 m |
16 ft 6 in |
25.56 m |
83 ft 1 |
wingspan |
11.72 m |
38 ft 5 in |
4 Rolls Royce/Snecma Olympus 593 turbo jet engines |
engines |
Two General Electric J79s |
18.7 tons (180 kN) |
thrust per engine |
17,900 lbs |
74.8 tons (720 kN) |
total thrust |
35,800 lbs |
185,000 kg |
408,000 lb |
MTOW |
27,965 kg |
61,700 lb |
6,580 km |
3,554 nm |
range |
3,031 km |
1,636 nm |
Mach 2.04 |
2,179 km/h |
cruise speed |
Mach 2.2 |
2,717 km/h |
92–120 passengers |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.