Northrop T-38 Talon vs. Short C-23 Sherpa

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Northrop T-38 Talon versus Short C-23 Sherpa
14.1 m 46 ft 4 in length 17.68 m 58 ft 0 in
3.9 m 12 ft 10 in height 6.55 m 21 ft 6 in
7.7 m 25 ft 3 in wingspan 22.76 m 74 ft 8 in
Two General Electric J85-GE-5A turbojet engines engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 1,200 hp per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 2,400 hp total
12,093 lb 5,485 kg MTOW 7,484 kg 16,500 lb
1,759 km 950 nm range 1,048 km 566 nm
745 kts 1,380 km/h cruise speed 425 km/h 264 mph
Two (student and instructor) capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.