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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.