Boeing 777-300ER vs. Lockheed Martin C-130J Super Hercules

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Boeing 777-300ER versus Lockheed Martin C-130J Super Hercules
73.9 m 242 ft 4 in length 34.37 m 112 ft 9 in
18.5 m 60 ft 8 in height 11.86 m 38 ft 11 in
64.8 m 212 ft 7 in wingspan 40.41 m 132 ft 7 in
GE90-115BL engines 4 x Rolls-Royce AE 2100D3 turboprop engines
115,300 lbf (513 kN) thrust per engine Approximately 4,700 hp per engine
230,600 lbf (1026 kN) total thrust Approximately 18,800 hp total
351,534 kg 775,000 lb MTOW 76,610 kg 168,900 lb
13,649 km 7,370 nmi range 4,600 km 2,485 nm
510 knots 945 km/h cruise speed 660 km/h 410 mph
396 passengers (2-class configuration) 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.