North American F-100 Super Sabre vs. Northrop T-38 Talon

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North American F-100 Super Sabre versus Northrop T-38 Talon
16.46 m 54 ft 2 in length 14.1 m 46 ft 4 in
4.93 m 16 ft 2 in height 3.9 m 12 ft 10 in
11.84 m 38 ft 1 wingspan 7.7 m 25 ft 3 in
1 Pratt & Whitney J57-P-21A engines Two General Electric J85-GE-5A turbojet engines
16,000 lb. thrust in afterburner thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
16,000 lb. (afterburner) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
17,609 kg 38,800 lb MTOW 12,093 lb 5,485 kg
2,673 km 1,444 nm range 1,759 km 950 nm
587 mph 945 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.