Airbus A300-600 vs. McDonnell Douglas F-4 Phantom II

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Airbus A300-600 versus McDonnell Douglas F-4 Phantom II
54.10 m 177 ft 6 in length 19.2 m 63 ft 0 in
16.5 m 54 ft 2 in height 5.03 m 16 ft 6 in
44.84 m 147 ft 1 in wingspan 11.72 m 38 ft 5 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines Two General Electric J79s
56,000lb to 61,500lb thrust per engine 17,900 lbs
112,000–123,000 lb total thrust 35,800 lbs
171,700 kg 378,600 lb MTOW 27,965 kg 61,700 lb
7,500 km 4,052 nm range 3,031 km 1,636 nm
897 km/h 557 mph cruise speed Mach 2.2 2,717 km/h
210-250 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.