BAC Jet Provost vs. Northrop T-38 Talon

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BAC Jet Provost versus Northrop T-38 Talon
10.36 m 34 ft 0 in length 14.1 m 46 ft 4 in
3.1 m 10 ft 2 in height 3.9 m 12 ft 10 in
11.25 m 36 ft 11 in wingspan 7.7 m 25 ft 3 in
1 x Bristol Siddeley Viper 201 engines Two General Electric J85-GE-5A turbojet engines
2,500 lb = 1,134 kg thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
2,500 lb = 1,134 kg total thrust 4,100 pounds dry thrust; 5,800 with afterburners
4,173 kg 9,200 lb MTOW 12,093 lb 5,485 kg
1,448 km 782 nm range 1,759 km 950 nm
440 mph 708 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.