Bombardier CRJ900 vs. Northrop T-38 Talon

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Bombardier CRJ900 versus Northrop T-38 Talon
36.2 m 118 ft 11 in length 14.1 m 46 ft 4 in
7.5 m 24 ft 7 in height 3.9 m 12 ft 10 in
24.9 m 81 ft 8 in wingspan 7.7 m 25 ft 3 in
2 Turbofans (fuselage mounted) engines Two General Electric J85-GE-5A turbojet engines
13,360 pounds force thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
26,720 pounds force total thrust 4,100 pounds dry thrust; 5,800 with afterburners
38,330 kg 84,500 lb MTOW 12,093 lb 5,485 kg
2,871 km 1,550 nm range 1,759 km 950 nm
515 mph 829 km/h cruise speed 745 kts 1,380 km/h
Up to 90 passengers 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.