Boeing 777-200 vs. Mil Mi-26
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Boeing 777-200 |
versus |
Mil Mi-26 |
63.7 m |
209 ft 1 in |
length |
40.03 m |
131.3 ft |
18.6 m |
61 ft |
height |
8.15 m |
26.7 ft |
64.8 m |
212 ft 7 in |
wingspan |
|
|
General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 |
engines |
2 x Lotarev D-136 turboshaft engines |
Up to 94,000 pounds |
thrust per engine |
8,380 kW |
Up to 188,000 pounds |
total thrust |
16,760 kW |
299,370 kg |
660,000 lb |
MTOW |
56,000 kg |
123,459 lb |
5,240 nm |
9,711 km |
range |
800 km |
432 nm |
560 mph |
901 km/h |
cruise speed |
255 km/h |
158 mph |
305 |
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.