McDonnell Douglas A-4 Skyhawk vs. Airbus A300-600F

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McDonnell Douglas A-4 Skyhawk versus Airbus A300-600F
12.19 m 40 ft 0 in length 54.08 m 177 ft 5 in
4.57 m 15 ft height 17.05 m 55 ft 11 in
8.08 m 26 ft 6 in wingspan 44.84 m 147 ft 1 in
1x Pratt & Whitney J52-P-6A Jet engines 2 x General Electric CF6-80C2A5 turbofan engines
8,500 pound-force thrust per engine Approximately 59,000 lbf per engine
8,500 pound-force total thrust Approximately 118,000 lbf total
11,113 kg 24,500 lb MTOW 170,000 kg 374,786 lb
3,222 km 1,739 nm range 4,830 km 2,608 nm
586 kts 364 mph cruise speed 860 km/h 534 mph
Up to 9,155 pounds of weapons on 5 hardpoints 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.