Airbus A350-800 vs. Lockheed Martin C-130J Super Hercules

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Airbus A350-800 versus Lockheed Martin C-130J Super Hercules
60.54 m 198 ft 7 in length 34.37 m 112 ft 9 in
17.05 m 55 ft 11 in height 11.86 m 38 ft 11 in
64.7 m 212 ft 5 in wingspan 40.41 m 132 ft 7 in
2 Turbofans (wing mounted) engines 4 x Rolls-Royce AE 2100D3 turboprop engines
75,760 lb thrust per engine Approximately 4,700 hp per engine
151,520 lb total thrust Approximately 18,800 hp total
283,000 kg 623,900 lb MTOW 76,610 kg 168,900 lb
11,708 km 6,319 nm range 4,600 km 2,485 nm
552 mph 888 km/h cruise speed 660 km/h 410 mph
Typically carries 300 to 350 passengers 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.