North American B-25 Mitchell vs. Northrop T-38 Talon

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North American B-25 Mitchell versus Northrop T-38 Talon
16.15 m 53 ft 0 in length 14.1 m 46 ft 4 in
5 m 16 ft 4 in height 3.9 m 12 ft 10 in
20.58 m 67 ft 6 in wingspan 7.7 m 25 ft 3 in
2 x Wright R-2600-92 Twin Cyclone engines Two General Electric J85-GE-5A turbojet engines
1,700 horsepower thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
3,400 horsepower total thrust 4,100 pounds dry thrust; 5,800 with afterburners
7,484 kg 16,500 lb MTOW 12,093 lb 5,485 kg
1,350 mi 1,175 nm range 1,759 km 950 nm
233 MPH 375 km/h cruise speed 745 kts 1,380 km/h
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.