North American F-100 Super Sabre vs. Lockheed Martin C-130J Super Hercules

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North American F-100 Super Sabre versus Lockheed Martin C-130J Super Hercules
16.46 m 54 ft 2 in length 34.37 m 112 ft 9 in
4.93 m 16 ft 2 in height 11.86 m 38 ft 11 in
11.84 m 38 ft 1 wingspan 40.41 m 132 ft 7 in
1 Pratt & Whitney J57-P-21A engines 4 x Rolls-Royce AE 2100D3 turboprop engines
16,000 lb. thrust in afterburner thrust per engine Approximately 4,700 hp per engine
16,000 lb. (afterburner) total thrust Approximately 18,800 hp total
17,609 kg 38,800 lb MTOW 76,610 kg 168,900 lb
2,673 km 1,444 nm range 4,600 km 2,485 nm
587 mph 945 km/h cruise speed 660 km/h 410 mph
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.