McDonnell Douglas F-4 Phantom II vs. Lockheed C-5 Galaxy

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McDonnell Douglas F-4 Phantom II versus Lockheed C-5 Galaxy
19.2 m 63 ft 0 in length 75.31 m 247 ft 2 in
5.03 m 16 ft 6 in height 19.84 m 65 ft 1 in
11.72 m 38 ft 5 in wingspan 67.89 m 222 ft 9 in
Two General Electric J79s engines 4 x General Electric TF39 turbofan engines
17,900 lbs thrust per engine 41,000 pounds of thrust (182 kilonewtons)
35,800 lbs total thrust 164,000 pounds
27,965 kg 61,700 lb MTOW 381,018 kg 840,000 lb
3,031 km 1,636 nm range 8,000 km 4,320 nm
Mach 2.2 2,717 km/h cruise speed 908 km/h 564 mph
Up to 16,000 lbs of externally carried ordnance capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.