McDonnell-Douglas MD-11 vs. Mil Mi-26
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McDonnell-Douglas MD-11 |
versus |
Mil Mi-26 |
61.20 m |
200 ft 10 in |
length |
40.03 m |
131.3 ft |
17.6 m |
57 ft 9 in |
height |
8.15 m |
26.7 ft |
51.6 m |
169 ft 4 in |
wingspan |
|
|
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
engines |
2 x Lotarev D-136 turboshaft engines |
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
thrust per engine |
8,380 kW |
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
total thrust |
16,760 kW |
285,990 kg |
630,400 lb |
MTOW |
56,000 kg |
123,459 lb |
13,231 km |
7,147 nm |
range |
800 km |
432 nm |
961 km/h |
597 mph |
cruise speed |
255 km/h |
158 mph |
Max 410 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.