Bombardier CS300 vs. Northrop T-38 Talon

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Bombardier CS300 versus Northrop T-38 Talon
38.0 m 124 ft 7 in length 14.1 m 46 ft 4 in
11.5 m 37 ft 9 in height 3.9 m 12 ft 10 in
35.1 m 115 ft 2 in wingspan 7.7 m 25 ft 3 in
2x Pratt & Whitney PurePower PW1000G engines Two General Electric J85-GE-5A turbojet engines
93.4 kN thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
186.8 kN total thrust 4,100 pounds dry thrust; 5,800 with afterburners
67,585 kg 149,000 lb MTOW 12,093 lb 5,485 kg
5,463 km 2,952 nm range 1,759 km 950 nm
871 km/h 541 mph cruise speed 745 kts 1,380 km/h
130 to 145 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.