McDonnell Douglas F-4 Phantom II vs. Lockheed Martin C-130J Super Hercules

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McDonnell Douglas F-4 Phantom II versus Lockheed Martin C-130J Super Hercules
19.2 m 63 ft 0 in length 34.37 m 112 ft 9 in
5.03 m 16 ft 6 in height 11.86 m 38 ft 11 in
11.72 m 38 ft 5 in wingspan 40.41 m 132 ft 7 in
Two General Electric J79s engines 4 x Rolls-Royce AE 2100D3 turboprop engines
17,900 lbs thrust per engine Approximately 4,700 hp per engine
35,800 lbs total thrust Approximately 18,800 hp total
27,965 kg 61,700 lb MTOW 76,610 kg 168,900 lb
3,031 km 1,636 nm range 4,600 km 2,485 nm
Mach 2.2 2,717 km/h cruise speed 660 km/h 410 mph
Up to 16,000 lbs of externally carried ordnance 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.