Bombardier CRJ700 vs. Northrop T-38 Talon

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Bombardier CRJ700 versus Northrop T-38 Talon
32.51 m 106 ft 8 in length 14.1 m 46 ft 4 in
7.6 m 24 ft 11 in height 3.9 m 12 ft 10 in
23.24 m 76 ft 3 in wingspan 7.7 m 25 ft 3 in
2 x General Electric CF34-8C5B1 turbofans engines Two General Electric J85-GE-5A turbojet engines
13,790 pounds (61.3 kN) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
27,580 pounds (122.6 kN) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
33,113 kg 73,000 lb MTOW 12,093 lb 5,485 kg
2,655 km 1,434 nm range 1,759 km 950 nm
514 mph 828 km/h cruise speed 745 kts 1,380 km/h
Up to 78 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.