Airbus A350-900ULR vs. Lockheed Martin C-130J Super Hercules

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Airbus A350-900ULR versus Lockheed Martin C-130J Super Hercules
66.80 m 219 ft 2 in length 34.37 m 112 ft 9 in
17.05 m 55 ft 11 in height 11.86 m 38 ft 11 in
64.75 m 212 ft 5 in wingspan 40.41 m 132 ft 7 in
2 Rolls-Royce Trent XWB engines 4 x Rolls-Royce AE 2100D3 turboprop engines
84,000 lbs thrust per engine Approximately 4,700 hp per engine
168,000 lbs total thrust Approximately 18,800 hp total
280,000 kg 617,300 lb MTOW 76,610 kg 168,900 lb
17,964 km 9,700 nm range 4,600 km 2,485 nm
552 mph 888 km/h cruise speed 660 km/h 410 mph
300-350 passengers in three classes 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.