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

versus
... or view the full comparison list here.
McDonnell Douglas F-4 Phantom II versus Airbus A300-600F
19.2 m 63 ft 0 in length 54.08 m 177 ft 5 in
5.03 m 16 ft 6 in height 17.05 m 55 ft 11 in
11.72 m 38 ft 5 in wingspan 44.84 m 147 ft 1 in
Two General Electric J79s engines 2 x General Electric CF6-80C2A5 turbofan engines
17,900 lbs thrust per engine Approximately 59,000 lbf per engine
35,800 lbs total thrust Approximately 118,000 lbf total
27,965 kg 61,700 lb MTOW 170,000 kg 374,786 lb
3,031 km 1,636 nm range 4,830 km 2,608 nm
Mach 2.2 2,717 km/h cruise speed 860 km/h 534 mph
Up to 16,000 lbs of externally carried ordnance capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.