Northrop T-38 Talon vs. de Havilland Canada DHC-6 Twin Otter

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Northrop T-38 Talon versus de Havilland Canada DHC-6 Twin Otter
14.1 m 46 ft 4 in length 15.32 m 50 ft 3 in
3.9 m 12 ft 10 in height 5.94 m 19 ft 6 in
7.7 m 25 ft 3 in wingspan 19.81 m 65 ft
Two General Electric J85-GE-5A turbojet engines engines 2 x Pratt & Whitney Canada PT6A-27 turboprop engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 550 to 750 shaft horsepower (410 to 560 kW)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 1100 to 1500 shaft horsepower
12,093 lb 5,485 kg MTOW 5,670 kg 12,500 lb
1,759 km 950 nm range 1,389 km 750 nm
745 kts 1,380 km/h cruise speed 280 km/h 174 mph
Two (student and instructor) capacity 19 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.