Bombardier CS100 vs. Lockheed Martin C-130J Super Hercules

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Bombardier CS100 versus Lockheed Martin C-130J Super Hercules
35.00 m 114 ft 10 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
2 x Pratt & Whitney PurePower PW1500G engines 4 x Rolls-Royce AE 2100D3 turboprop engines
84.1 kN thrust per engine Approximately 4,700 hp per engine
168.2 kN total thrust Approximately 18,800 hp total
54,931 kg 121,100 lb MTOW 76,610 kg 168,900 lb
4,074 km 2,200 nm range 4,600 km 2,485 nm
871 km/h 541 mph cruise speed 660 km/h 410 mph
110 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.