North American BT-9 vs. Northrop T-38 Talon

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North American BT-9 versus Northrop T-38 Talon
8.79 m 28 ft 10 in length 14.1 m 46 ft 4 in
2.82 m 9 ft 3 in height 3.9 m 12 ft 10 in
10.97 m 36 ft wingspan 7.7 m 25 ft 3 in
1 x Wright R-975-3 radial engine engines Two General Electric J85-GE-5A turbojet engines
Approximately 440 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 440 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
4,300 lb 1,950 kg MTOW 12,093 lb 5,485 kg
917 km 495 nm range 1,759 km 950 nm
150 mph 241 km/h cruise speed 745 kts 1,380 km/h
Pilot and one passenger 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.