Northrop T-38 Talon vs. Percival Provost

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Northrop T-38 Talon versus Percival Provost
14.1 m 46 ft 4 in length 9.0 m 29 ft 6 in
3.9 m 12 ft 10 in height 3.02 m 9 ft 11 in
7.7 m 25 ft 3 in wingspan 12.19 m 40 ft
Two General Electric J85-GE-5A turbojet engines engines 1 x Alvis Leonides Major 755/1 inline engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 550 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 550 hp
12,093 lb 5,485 kg MTOW 5,500 lb 2,495 kg
1,759 km 950 nm range 1,127 km 608 nm
745 kts 1,380 km/h cruise speed 175 mph 282 km/h
Two (student and instructor) capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.