Airbus A330-300 vs. McDonnell Douglas F-4 Phantom II

versus
... or view the full comparison list here.
Airbus A330-300 versus McDonnell Douglas F-4 Phantom II
63.66 m 208 ft 9 in length 19.2 m 63 ft 0 in
16.79 m 55 ft 1 in height 5.03 m 16 ft 6 in
60.3 m 197 ft 9 in wingspan 11.72 m 38 ft 5 in
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines Two General Electric J79s
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 17,900 lbs
Depends on the engine type total thrust 35,800 lbs
242,000 kg 533,600 lb MTOW 27,965 kg 61,700 lb
11,750 km 6,346 nm range 3,031 km 1,636 nm
900 km/h 559 mph cruise speed Mach 2.2 2,717 km/h
250-290 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.