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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.