Boeing 737-200 vs. McDonnell Douglas F-4 Phantom II

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Boeing 737-200 versus McDonnell Douglas F-4 Phantom II
30.53 m 100 ft 2 in length 19.2 m 63 ft 0 in
11.23 m 36 ft 10 in height 5.03 m 16 ft 6 in
28.35 m 93 ft wingspan 11.72 m 38 ft 5 in
2 Turbofan Engines engines Two General Electric J79s
71.2 kN thrust per engine 17,900 lbs
142.4 kN total thrust 35,800 lbs
52,390 kg 115,500 lb MTOW 27,965 kg 61,700 lb
4,899 km 2,646 nm range 3,031 km 1,636 nm
933 km/h 580 mph cruise speed Mach 2.2 2,717 km/h
97 / 124 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.