Lockheed Martin F-35 Lightning II vs. McDonnell Douglas A-4 Skyhawk

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Lockheed Martin F-35 Lightning II versus McDonnell Douglas A-4 Skyhawk
15.67 m 51 ft 4 in length 12.19 m 40 ft 0 in
4.33 m 14 ft 2 in height 4.57 m 15 ft
10.7 m 35 ft 1 in wingspan 8.08 m 26 ft 6 in
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 1x Pratt & Whitney J52-P-6A Jet
40,000 lb thrust per engine 8,500 pound-force
40,000 lb total thrust 8,500 pound-force
31,800 kg 70,000 lb MTOW 11,113 kg 24,500 lb
1,380 mi 1,200 nm range 3,222 km 1,739 nm
520 kt 302 mph cruise speed 586 kts 364 mph
18,000 pounds of total ordinance 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.