de Havilland Canada DHC-2 Beaver vs. Antonov An-124 Ruslan
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de Havilland Canada DHC-2 Beaver |
versus |
Antonov An-124 Ruslan |
13.56 m |
44 ft 6 in |
length |
69.10 m |
226 ft 9 in |
5 m |
16 ft 5 in |
height |
20.78 m |
68 ft 2 in |
16.56 m |
54 ft 4 in |
wingspan |
73.3 m |
240 ft 6 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
4 x Ivchenko Progress D-18T turbofan engines |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 51,590 lbf |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 206,360 lbf |
24,200 lb |
10,977 kg |
MTOW |
405,000 kg |
893,000 lb |
2,535 km |
1,369 nm |
range |
3,700 km |
1,998 nm |
228 mph |
367 km/h |
cruise speed |
800 km/h |
497 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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.