Bombardier CRJ1000 vs. Northrop T-38 Talon

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Bombardier CRJ1000 versus Northrop T-38 Talon
39.1 m 128 ft 5 in length 14.1 m 46 ft 4 in
7.5 m 24 ft 7 in height 3.9 m 12 ft 10 in
26.2 m 86 ft wingspan 7.7 m 25 ft 3 in
2 GE CF34-8C5A1 turbofans engines Two General Electric J85-GE-5A turbojet engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 4,100 pounds dry thrust; 5,800 with afterburners
41,640 kg 91,800 lb MTOW 12,093 lb 5,485 kg
3,004 km 1,623 nm range 1,759 km 950 nm
515 mph 829 km/h cruise speed 745 kts 1,380 km/h
100 (common) 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.