Nanchang CJ-6 vs. Northrop T-38 Talon

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Nanchang CJ-6 versus Northrop T-38 Talon
8.48 m 27 ft 10 in length 14.1 m 46 ft 4 in
2.67 m 8 ft 9 in height 3.9 m 12 ft 10 in
10.49 m 34 ft 5 in wingspan 7.7 m 25 ft 3 in
1 x Ivchenko AI-14RA radial engine engines Two General Electric J85-GE-5A turbojet engines
Approximately 260 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 260 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
3,858 lb 1,751 kg MTOW 12,093 lb 5,485 kg
800 km 432 nm range 1,759 km 950 nm
155 mph 249 km/h cruise speed 745 kts 1,380 km/h
Pilot and one passenger 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.