Airbus A310-300 vs. McDonnell Douglas F-4 Phantom II

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Airbus A310-300 versus McDonnell Douglas F-4 Phantom II
46.66 m 153 ft 1 in length 19.2 m 63 ft 0 in
15.8 m 51 ft 10 in height 5.03 m 16 ft 6 in
43.9 m 144 ft wingspan 11.72 m 38 ft 5 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Two General Electric J79s
52,000 lb thrust per engine 17,900 lbs
104,000 lb total thrust 35,800 lbs
148,768 kg 328,000 lb MTOW 27,965 kg 61,700 lb
8,050 km 4,348 nm range 3,031 km 1,636 nm
482 knots 279 mph cruise speed Mach 2.2 2,717 km/h
190-230 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.