North American B-25 Mitchell vs. Lockheed Martin C-130J Super Hercules

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North American B-25 Mitchell versus Lockheed Martin C-130J Super Hercules
16.15 m 53 ft 0 in length 34.37 m 112 ft 9 in
5 m 16 ft 4 in height 11.86 m 38 ft 11 in
20.58 m 67 ft 6 in wingspan 40.41 m 132 ft 7 in
2 x Wright R-2600-92 Twin Cyclone engines 4 x Rolls-Royce AE 2100D3 turboprop engines
1,700 horsepower thrust per engine Approximately 4,700 hp per engine
3,400 horsepower total thrust Approximately 18,800 hp total
7,484 kg 16,500 lb MTOW 76,610 kg 168,900 lb
1,350 mi 1,175 nm range 4,600 km 2,485 nm
233 MPH 375 km/h cruise speed 660 km/h 410 mph
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.