McDonnell-Douglas DC-9-30 vs. McDonnell Douglas F-4 Phantom II

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McDonnell-Douglas DC-9-30 versus McDonnell Douglas F-4 Phantom II
36.36 m 119 ft 3 in length 19.2 m 63 ft 0 in
8.5 m 27 ft 11 in height 5.03 m 16 ft 6 in
28.44 m 93 ft 4 in wingspan 11.72 m 38 ft 5 in
2x Pratt & Whitney JT8D engines Two General Electric J79s
15,000 pound-force thrust per engine 17,900 lbs
30,000 pound-force (2 engines) total thrust 35,800 lbs
54,885 kg 121,000 lb MTOW 27,965 kg 61,700 lb
2,632 km 1,422 nm range 3,031 km 1,636 nm
898 km/h 558 mph cruise speed Mach 2.2 2,717 km/h
Up to 139 passengers 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.