Airbus A330-300 vs. Mil Mi-26
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Airbus A330-300 |
versus |
Mil Mi-26 |
63.66 m |
208 ft 9 in |
length |
40.03 m |
131.3 ft |
16.79 m |
55 ft 1 in |
height |
8.15 m |
26.7 ft |
60.3 m |
197 ft 9 in |
wingspan |
|
|
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
2 x Lotarev D-136 turboshaft engines |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
8,380 kW |
Depends on the engine type |
total thrust |
16,760 kW |
242,000 kg |
533,600 lb |
MTOW |
56,000 kg |
123,459 lb |
11,750 km |
6,346 nm |
range |
800 km |
432 nm |
900 km/h |
559 mph |
cruise speed |
255 km/h |
158 mph |
250-290 |
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.