Lockheed L-1011 TriStar 500 vs. McDonnell Douglas A-4 Skyhawk

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Lockheed L-1011 TriStar 500 versus McDonnell Douglas A-4 Skyhawk
50.05 m 164 ft 3 in length 12.19 m 40 ft 0 in
16.87 m 55 ft 4 in height 4.57 m 15 ft
50.09 m 164 ft 4 in wingspan 8.08 m 26 ft 6 in
3 Rolls-Royce RB211 engines engines 1x Pratt & Whitney J52-P-6A Jet
42,000 lbf thrust per engine 8,500 pound-force
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 8,500 pound-force
231,330 kg 510,000 lb MTOW 11,113 kg 24,500 lb
11,260 km 6,100 nm range 3,222 km 1,739 nm
525 knots 972 km/h cruise speed 586 kts 364 mph
Max. 315 passengers (typical 253) 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.