McDonnell-Douglas DC-10-30 vs. McDonnell Douglas F-4 Phantom II

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McDonnell-Douglas DC-10-30 versus McDonnell Douglas F-4 Phantom II
55.35 m 181 ft 8 in length 19.2 m 63 ft 0 in
17.8 m 58 ft 5 in height 5.03 m 16 ft 6 in
50.39 m 165 ft 4 in wingspan 11.72 m 38 ft 5 in
3x GE CF6-50C Turbofan engines Two General Electric J79s
54,000 lbf thrust per engine 17,900 lbs
162,000 lbf total thrust 35,800 lbs
251,744 kg 555,000 lb MTOW 27,965 kg 61,700 lb
9,630 km 5,200 nm range 3,031 km 1,636 nm
507 knots 939 km/h cruise speed Mach 2.2 2,717 km/h
Up to 380 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.