Bombardier CS100 vs. Northrop T-38 Talon

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Bombardier CS100 versus Northrop T-38 Talon
35.00 m 114 ft 10 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
2 x Pratt & Whitney PurePower PW1500G engines Two General Electric J85-GE-5A turbojet engines
84.1 kN thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
168.2 kN total thrust 4,100 pounds dry thrust; 5,800 with afterburners
54,931 kg 121,100 lb MTOW 12,093 lb 5,485 kg
4,074 km 2,200 nm range 1,759 km 950 nm
871 km/h 541 mph cruise speed 745 kts 1,380 km/h
110 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.