Chengdu J-20 vs. Northrop T-38 Talon

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Chengdu J-20 versus Northrop T-38 Talon
20.4 m 66 ft 11 in length 14.1 m 46 ft 4 in
4.45 m 14 ft 7 in height 3.9 m 12 ft 10 in
13.01 m 42 ft 8 in wingspan 7.7 m 25 ft 3 in
2x Saturn 117S or Xian WS-15 engines Two General Electric J85-GE-5A turbojet engines
30,000-32,000 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
60,000-64,000 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
37,000 kg 81,600 lb MTOW 12,093 lb 5,485 kg
3,200 nm 5,926 km range 1,759 km 950 nm
1,305 mph 2,100 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.