de Havilland Canada DHC-2 Beaver vs. Lockheed Martin C-130J Super Hercules

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de Havilland Canada DHC-2 Beaver versus Lockheed Martin C-130J Super Hercules
13.56 m 44 ft 6 in length 34.37 m 112 ft 9 in
5 m 16 ft 5 in height 11.86 m 38 ft 11 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 Rolls-Royce AE 2100D3 turboprop engines
Approximately 3,100 hp (2,312 kW) each thrust per engine Approximately 4,700 hp per engine
Approximately 6,200 hp (4,624 kW) total total thrust Approximately 18,800 hp total
24,200 lb 10,977 kg MTOW 76,610 kg 168,900 lb
2,535 km 1,369 nm range 4,600 km 2,485 nm
228 mph 367 km/h cruise speed 660 km/h 410 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.