de Havilland Canada DHC-2 Beaver vs. Mil Mi-26
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here.
de Havilland Canada DHC-2 Beaver |
versus |
Mil Mi-26 |
13.56 m |
44 ft 6 in |
length |
40.03 m |
131.3 ft |
5 m |
16 ft 5 in |
height |
8.15 m |
26.7 ft |
16.56 m |
54 ft 4 in |
wingspan |
|
|
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
2 x Lotarev D-136 turboshaft engines |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
8,380 kW |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
16,760 kW |
24,200 lb |
10,977 kg |
MTOW |
56,000 kg |
123,459 lb |
2,535 km |
1,369 nm |
range |
800 km |
432 nm |
228 mph |
367 km/h |
cruise speed |
255 km/h |
158 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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.