Concorde vs. Airbus H225 Super Puma
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Concorde |
versus |
Airbus H225 Super Puma |
61.66 m |
202 ft 4 in |
length |
14.06 m |
46 ft 2 in |
11.4 m |
37 ft 5 in |
height |
4.38 m |
14 ft 4 in |
25.56 m |
83 ft 1 |
wingspan |
|
|
4 Rolls Royce/Snecma Olympus 593 turbo jet engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
18.7 tons (180 kN) |
thrust per engine |
2,778 hp |
74.8 tons (720 kN) |
total thrust |
5,556 hp |
185,000 kg |
408,000 lb |
MTOW |
11,000 kg |
24,251 lb |
6,580 km |
3,554 nm |
range |
857 km |
463 nm |
Mach 2.04 |
2,179 km/h |
cruise speed |
242 km/h |
150 mph |
92–120 passengers |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.