Lockheed Martin F-22 Raptor vs. McDonnell Douglas F-4 Phantom II

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Lockheed Martin F-22 Raptor versus McDonnell Douglas F-4 Phantom II
18.9 m 62 ft 1 in length 19.2 m 63 ft 0 in
5.1 m 16 ft 9 in height 5.03 m 16 ft 6 in
13.6 m 44 ft 7 in wingspan 11.72 m 38 ft 5 in
Two Pratt & Whitney F119-PW-100 turbofan engines engines Two General Electric J79s
35,000-pound class thrust per engine 17,900 lbs
70,000-pound class total thrust 35,800 lbs
38,000 kg 83,500 lb MTOW 27,965 kg 61,700 lb
1,850 mi 1,611 nm range 3,031 km 1,636 nm
Mach 1.6 1976 km/h cruise speed Mach 2.2 2,717 km/h
capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.