McDonnell-Douglas MD-11 vs. McDonnell Douglas F-4 Phantom II

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McDonnell-Douglas MD-11 versus McDonnell Douglas F-4 Phantom II
61.20 m 200 ft 10 in length 19.2 m 63 ft 0 in
17.6 m 57 ft 9 in height 5.03 m 16 ft 6 in
51.6 m 169 ft 4 in wingspan 11.72 m 38 ft 5 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines Two General Electric J79s
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 17,900 lbs
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 35,800 lbs
285,990 kg 630,400 lb MTOW 27,965 kg 61,700 lb
13,231 km 7,147 nm range 3,031 km 1,636 nm
961 km/h 597 mph cruise speed Mach 2.2 2,717 km/h
Max 410 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.