Bombardier CRJ1000 vs. Antonov An-124 Ruslan

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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.