Bombardier CRJ1000 vs. Antonov An-124 Ruslan
... or view the full comparison list
here.
Bombardier CRJ1000 |
versus |
Antonov An-124 Ruslan |
39.1 m |
128 ft 5 in |
length |
69.10 m |
226 ft 9 in |
7.5 m |
24 ft 7 in |
height |
20.78 m |
68 ft 2 in |
26.2 m |
86 ft |
wingspan |
73.3 m |
240 ft 6 in |
2 GE CF34-8C5A1 turbofans |
engines |
4 x Ivchenko Progress D-18T turbofan 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 |
Approximately 51,590 lbf |
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 |
Approximately 206,360 lbf |
41,640 kg |
91,800 lb |
MTOW |
405,000 kg |
893,000 lb |
3,004 km |
1,623 nm |
range |
3,700 km |
1,998 nm |
515 mph |
829 km/h |
cruise speed |
800 km/h |
497 mph |
100 (common) |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.