McDonnell Douglas A-4 Skyhawk vs. Northrop T-38 Talon

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McDonnell Douglas A-4 Skyhawk versus Northrop T-38 Talon
12.19 m 40 ft 0 in length 14.1 m 46 ft 4 in
4.57 m 15 ft height 3.9 m 12 ft 10 in
8.08 m 26 ft 6 in wingspan 7.7 m 25 ft 3 in
1x Pratt & Whitney J52-P-6A Jet engines Two General Electric J85-GE-5A turbojet engines
8,500 pound-force thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
8,500 pound-force total thrust 4,100 pounds dry thrust; 5,800 with afterburners
11,113 kg 24,500 lb MTOW 12,093 lb 5,485 kg
3,222 km 1,739 nm range 1,759 km 950 nm
586 kts 364 mph cruise speed 745 kts 1,380 km/h
Up to 9,155 pounds of weapons on 5 hardpoints capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.