Antonov An-124 Ruslan vs. Canadair CL-415
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Antonov An-124 Ruslan |
versus |
Canadair CL-415 |
69.10 m |
226 ft 9 in |
length |
19.82 m |
65 ft 0 in |
20.78 m |
68 ft 2 in |
height |
8.66 m |
28 ft 5 in |
73.3 m |
240 ft 6 in |
wingspan |
28.6 m |
93 ft 1 |
4 x Ivchenko Progress D-18T turbofan engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
Approximately 51,590 lbf |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
Approximately 206,360 lbf |
total thrust |
4,300 to 4,760 shaft horsepower |
405,000 kg |
893,000 lb |
MTOW |
19,733 kg |
43,525 lb |
3,700 km |
1,998 nm |
range |
1,600 km |
864 nm |
800 km/h |
497 mph |
cruise speed |
290 km/h |
180 mph |
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capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.