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

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Airbus A300-600 versus McDonnell Douglas A-4 Skyhawk
54.10 m 177 ft 6 in length 12.19 m 40 ft 0 in
16.5 m 54 ft 2 in height 4.57 m 15 ft
44.84 m 147 ft 1 in wingspan 8.08 m 26 ft 6 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1x Pratt & Whitney J52-P-6A Jet
56,000lb to 61,500lb thrust per engine 8,500 pound-force
112,000–123,000 lb total thrust 8,500 pound-force
171,700 kg 378,600 lb MTOW 11,113 kg 24,500 lb
7,500 km 4,052 nm range 3,222 km 1,739 nm
897 km/h 557 mph cruise speed 586 kts 364 mph
210-250 passengers capacity Up to 9,155 pounds of weapons on 5 hardpoints
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.