Northrop T-38 Talon vs. Beechcraft T-6 Texan II

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Northrop T-38 Talon versus Beechcraft T-6 Texan II
14.1 m 46 ft 4 in length 10.18 m 33 ft 4 in
3.9 m 12 ft 10 in height 3.29 m 10 ft 10 in
7.7 m 25 ft 3 in wingspan 10.21 m 33 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 1 x Pratt & Whitney Canada PT6A-68
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 1100 lbs
4,100 pounds dry thrust; 5,800 with afterburners total thrust 1100 lbs
12,093 lb 5,485 kg MTOW 6,250 lb 2,835 kg
1,759 km 950 nm range 900 nm 1,667 km
745 kts 1,380 km/h cruise speed 320 kts 199 mph
Two (student and instructor) capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.