Northrop T-38 Talon vs. Air Tractor AT-802

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Northrop T-38 Talon versus Air Tractor AT-802
14.1 m 46 ft 4 in length 10.16 m 33 ft 4 in
3.9 m 12 ft 10 in height 3.66 m 12 ft
7.7 m 25 ft 3 in wingspan 18.29 m 60 ft
Two General Electric J85-GE-5A turbojet engines engines 1 x Pratt & Whitney Canada PT6A-67F turboprop engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
12,093 lb 5,485 kg MTOW 7,257 kg 16,000 lb
1,759 km 950 nm range 1,125 km 607 nm
745 kts 1,380 km/h cruise speed 240 km/h 149 mph
Two (student and instructor) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.