Lockheed Martin F-35 Lightning II vs. Northrop T-38 Talon

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Lockheed Martin F-35 Lightning II versus Northrop T-38 Talon
15.67 m 51 ft 4 in length 14.1 m 46 ft 4 in
4.33 m 14 ft 2 in height 3.9 m 12 ft 10 in
10.7 m 35 ft 1 in wingspan 7.7 m 25 ft 3 in
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines Two General Electric J85-GE-5A turbojet engines
40,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
40,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
31,800 kg 70,000 lb MTOW 12,093 lb 5,485 kg
1,380 mi 1,200 nm range 1,759 km 950 nm
520 kt 302 mph cruise speed 745 kts 1,380 km/h
18,000 pounds of total ordinance 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.