Northrop T-38 Talon vs. de Havilland Canada DHC-3 Otter

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Northrop T-38 Talon versus de Havilland Canada DHC-3 Otter
14.1 m 46 ft 4 in length 10.52 m 34 ft 6 in
3.9 m 12 ft 10 in height 3.84 m 12 ft 7 in
7.7 m 25 ft 3 in wingspan 17.68 m 58 ft
Two General Electric J85-GE-5A turbojet engines engines 1 x Pratt & Whitney R-1340 radial engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 400 to 600 horsepower (298 to 447 kW)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 400 to 600 horsepower (298 to 447 kW)
12,093 lb 5,485 kg MTOW 5,670 kg 12,500 lb
1,759 km 950 nm range 1,296 km 700 nm
745 kts 1,380 km/h cruise speed 215 km/h 134 mph
Two (student and instructor) capacity 10-11 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.