Lockheed P-38 Lightning vs. Northrop T-38 Talon

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Lockheed P-38 Lightning versus Northrop T-38 Talon
11.53 m 37 ft 10 in length 14.1 m 46 ft 4 in
3.91 m 12 ft 10 in height 3.9 m 12 ft 10 in
15.85 m 52 ft wingspan 7.7 m 25 ft 3 in
Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines engines Two General Electric J85-GE-5A turbojet engines
1,425 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
2,850 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
9,798 kg 21,600 lb MTOW 12,093 lb 5,485 kg
1,100 nm 2,037 km range 1,759 km 950 nm
239 knots 139 mph cruise speed 745 kts 1,380 km/h
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.