Concorde vs. Mil Mi-26
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Concorde |
versus |
Mil Mi-26 |
61.66 m |
202 ft 4 in |
length |
40.03 m |
131.3 ft |
11.4 m |
37 ft 5 in |
height |
8.15 m |
26.7 ft |
25.56 m |
83 ft 1 |
wingspan |
|
|
4 Rolls Royce/Snecma Olympus 593 turbo jet engines |
engines |
2 x Lotarev D-136 turboshaft engines |
18.7 tons (180 kN) |
thrust per engine |
8,380 kW |
74.8 tons (720 kN) |
total thrust |
16,760 kW |
185,000 kg |
408,000 lb |
MTOW |
56,000 kg |
123,459 lb |
6,580 km |
3,554 nm |
range |
800 km |
432 nm |
Mach 2.04 |
2,179 km/h |
cruise speed |
255 km/h |
158 mph |
92–120 passengers |
capacity |
Up to 90 passengers |
|
|
rotor diameter |
32.00 m |
105 ft 0 in |
|
|
rate of climb |
8 m/s |
1,574 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.