McDonnell Douglas F-4 Phantom II vs. North American P-51 Mustang

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McDonnell Douglas F-4 Phantom II versus North American P-51 Mustang
19.2 m 63 ft 0 in length 9.83 m 32 ft 3 in
5.03 m 16 ft 6 in height 4.08 m 13 ft 5 in
11.72 m 38 ft 5 in wingspan 11.28 m 37 ft
Two General Electric J79s engines Packard Rolls Royce Merlin V-1650-7
17,900 lbs thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
35,800 lbs total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
27,965 kg 61,700 lb MTOW 5,489 kg 12,100 lb
3,031 km 1,636 nm range 2,200 km 1,188 nm
Mach 2.2 2,717 km/h cruise speed 325 mph 525 km/h
Up to 16,000 lbs of externally carried ordnance capacity 2,000 pounds of bombs, or ten 5-inch rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.