Folland Gnat vs. Northrop T-38 Talon

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Folland Gnat versus Northrop T-38 Talon
9.67 m 31 ft 9 in length 14.1 m 46 ft 4 in
2.95 m 9 ft 8 in height 3.9 m 12 ft 10 in
7.32 m 24 ft wingspan 7.7 m 25 ft 3 in
Bristol Siddeley Orpheus 100 engines Two General Electric J85-GE-5A turbojet engines
4700 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
4700 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
3,915 kg 8,630 lb MTOW 12,093 lb 5,485 kg
1,851 km 999 nm range 1,759 km 950 nm
360 mph 579 km/h cruise speed 745 kts 1,380 km/h
Single or two-seat light fighter and trainer aircraft 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.