Comac ARJ21-900ER vs. Northrop T-38 Talon

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Comac ARJ21-900ER versus Northrop T-38 Talon
36.40 m 119 ft 5 in length 14.1 m 46 ft 4 in
8.4 m 27 ft 7 in height 3.9 m 12 ft 10 in
27.3 m 89 ft 7 in wingspan 7.7 m 25 ft 3 in
2 General Electric CF34-10A engines engines Two General Electric J85-GE-5A turbojet engines
17,057 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
34,114 lbf total thrust 4,100 pounds dry thrust; 5,800 with afterburners
47,182 kg 104,000 lb MTOW 12,093 lb 5,485 kg
2,225 km 1,202 nm range 1,759 km 950 nm
Mach 0.78 963 km/h cruise speed 745 kts 1,380 km/h
78 to 97 seats 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.