Bombardier CS300 vs. Lockheed Martin C-130J Super Hercules

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Bombardier CS300 versus Lockheed Martin C-130J Super Hercules
38.0 m 124 ft 7 in length 34.37 m 112 ft 9 in
11.5 m 37 ft 9 in height 11.86 m 38 ft 11 in
35.1 m 115 ft 2 in wingspan 40.41 m 132 ft 7 in
2x Pratt & Whitney PurePower PW1000G engines 4 x Rolls-Royce AE 2100D3 turboprop engines
93.4 kN thrust per engine Approximately 4,700 hp per engine
186.8 kN total thrust Approximately 18,800 hp total
67,585 kg 149,000 lb MTOW 76,610 kg 168,900 lb
5,463 km 2,952 nm range 4,600 km 2,485 nm
871 km/h 541 mph cruise speed 660 km/h 410 mph
130 to 145 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.