Embraer E175-E2 vs. Northrop T-38 Talon

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Embraer E175-E2 versus Northrop T-38 Talon
29.94 m 98 ft 2 in length 14.1 m 46 ft 4 in
9.81 m 32 ft 2 in height 3.9 m 12 ft 10 in
28.7 m 94 ft 2 in wingspan 7.7 m 25 ft 3 in
2 (Pratt & Whitney Pure Power Geared Turbofan engines) engines Two General Electric J85-GE-5A turbojet engines
67 kN thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
134 kN total thrust 4,100 pounds dry thrust; 5,800 with afterburners
44,800 kg 98,800 lb MTOW 12,093 lb 5,485 kg
3,815 km 2,060 nm range 1,759 km 950 nm
M 0.82 101,3 km/h cruise speed 745 kts 1,380 km/h
Three classes configuration: 80 seats (12 at 36”, 16 at 34”, 52 at 30”); Single class configuration: 88 seats at 31” or 90 seats (50 at 30”, 40 at 29”) 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.