de Havilland Canada DHC-2 Beaver vs. lockheed C-130 hercules
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de Havilland Canada DHC-2 Beaver |
versus |
lockheed C-130 hercules |
13.56 m |
44 ft 6 in |
length |
29.79 m |
97 ft 9 in |
5 m |
16 ft 5 in |
height |
11.66 m |
38 ft 3 in |
16.56 m |
54 ft 4 in |
wingspan |
40.41 m |
132 ft 7 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
4 x Allison T56-A-15 turboprop engines |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 4,590 hp per engine |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 18,360 hp total |
24,200 lb |
10,977 kg |
MTOW |
70,307 kg |
155,000 lb |
2,535 km |
1,369 nm |
range |
3,760 km |
2,031 nm |
228 mph |
367 km/h |
cruise speed |
540 km/h |
335 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
based on configuration |
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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.