Boeing F/A-18E/F Super Hornet vs. Lockheed Martin C-130J Super Hercules

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Boeing F/A-18E/F Super Hornet versus Lockheed Martin C-130J Super Hercules
18.5 m 60 ft 3 in length 34.37 m 112 ft 9 in
4.87 m 16 ft height 11.86 m 38 ft 11 in
13.68 m 44 ft 1 wingspan 40.41 m 132 ft 7 in
Two F414-GE-400 turbofan engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Up to 17,000 lbs thrust per engine Approximately 4,700 hp per engine
Up to 34,000 lbs total thrust Approximately 18,800 hp total
29,937 kg 66,000 lb MTOW 76,610 kg 168,900 lb
2,346 km 1,268 nm range 4,600 km 2,485 nm
1032 knots 1,911 km/h cruise speed 660 km/h 410 mph
Overall capability across all eleven hardpoints is 17,750lbs of external stores 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.