Bombardier CRJ1000 vs. Mil Mi-26
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here.
Bombardier CRJ1000 |
versus |
Mil Mi-26 |
39.1 m |
128 ft 5 in |
length |
40.03 m |
131.3 ft |
7.5 m |
24 ft 7 in |
height |
8.15 m |
26.7 ft |
26.2 m |
86 ft |
wingspan |
|
|
2 GE CF34-8C5A1 turbofans |
engines |
2 x Lotarev D-136 turboshaft engines |
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve |
thrust per engine |
8,380 kW |
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
total thrust |
16,760 kW |
41,640 kg |
91,800 lb |
MTOW |
56,000 kg |
123,459 lb |
3,004 km |
1,623 nm |
range |
800 km |
432 nm |
515 mph |
829 km/h |
cruise speed |
255 km/h |
158 mph |
100 (common) |
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.