Northrop T-38 Talon vs. Short 360

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Northrop T-38 Talon versus Short 360
14.1 m 46 ft 4 in length 17.74 m 58 ft 2 in
3.9 m 12 ft 10 in height 6.8 m 22 ft 4 in
7.7 m 25 ft 3 in wingspan 22.72 m 74 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 2 x Pratt & Whitney Canada PT6A-65R
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 2,430 lbs
4,100 pounds dry thrust; 5,800 with afterburners total thrust 4,860 lbs
12,093 lb 5,485 kg MTOW 28,400 lb 12,882 kg
1,759 km 950 nm range 820 nm 1,519 km
745 kts 1,380 km/h cruise speed 220 kts 137 mph
Two (student and instructor) capacity 36
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.