McDonnell Douglas F-4 Phantom II vs. lockheed C-130 hercules

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McDonnell Douglas F-4 Phantom II versus lockheed C-130 hercules
19.2 m 63 ft 0 in length 29.79 m 97 ft 9 in
5.03 m 16 ft 6 in height 11.66 m 38 ft 3 in
11.72 m 38 ft 5 in wingspan 40.41 m 132 ft 7 in
Two General Electric J79s engines 4 x Allison T56-A-15 turboprop engines
17,900 lbs thrust per engine Approximately 4,590 hp per engine
35,800 lbs total thrust Approximately 18,360 hp total
27,965 kg 61,700 lb MTOW 70,307 kg 155,000 lb
3,031 km 1,636 nm range 3,760 km 2,031 nm
Mach 2.2 2,717 km/h cruise speed 540 km/h 335 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.