Lockheed U-2 vs. McDonnell Douglas F-4 Phantom II

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Lockheed U-2 versus McDonnell Douglas F-4 Phantom II
19.2 m 63 ft 0 in length 19.2 m 63 ft 0 in
4.8 m 15 ft 9 in height 5.03 m 16 ft 6 in
32 m 105 ft wingspan 11.72 m 38 ft 5 in
1 × General Electric F118-101 engines Two General Electric J79s
17,000 lbf (76 kN) thrust per engine 17,900 lbs
17,000 lbf (76 kN) total thrust 35,800 lbs
18,144 kg 40,000 lb MTOW 27,965 kg 61,700 lb
6,090 nm 11,278 km range 3,031 km 1,636 nm
475 mph 764 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.