Boeing 747-8I vs. Mil Mi-26
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Boeing 747-8I |
versus |
Mil Mi-26 |
76.25 m |
250 ft 2 in |
length |
40.03 m |
131.3 ft |
19.35 m |
63 ft 6 in |
height |
8.15 m |
26.7 ft |
68.45 m |
224 ft 7 in |
wingspan |
|
|
4x General Electric GEnx 2B67 Turbofan |
engines |
2 x Lotarev D-136 turboshaft engines |
66,500 pounds |
thrust per engine |
8,380 kW |
266,000 pounds |
total thrust |
16,760 kW |
443,613 kg |
977,500 lb |
MTOW |
56,000 kg |
123,459 lb |
8,000 nm |
14,816 km |
range |
800 km |
432 nm |
Mach 0.86 |
1,062 km/h |
cruise speed |
255 km/h |
158 mph |
467 passengers (three-class configuration) |
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.