Lockheed U-2 vs. Northrop T-38 Talon

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Lockheed U-2 versus Northrop T-38 Talon
19.2 m 63 ft 0 in length 14.1 m 46 ft 4 in
4.8 m 15 ft 9 in height 3.9 m 12 ft 10 in
32 m 105 ft wingspan 7.7 m 25 ft 3 in
1 × General Electric F118-101 engines Two General Electric J85-GE-5A turbojet engines
17,000 lbf (76 kN) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
17,000 lbf (76 kN) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
18,144 kg 40,000 lb MTOW 12,093 lb 5,485 kg
6,090 nm 11,278 km range 1,759 km 950 nm
475 mph 764 km/h 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.