Northrop T-38 Talon vs. Aero Commander 520

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Northrop T-38 Talon versus Aero Commander 520
14.1 m 46 ft 4 in length 11.18 m 36 ft 8 in
3.9 m 12 ft 10 in height 3.45 m 11 ft 4 in
7.7 m 25 ft 3 in wingspan 14.28 m 46 ft 1
Two General Electric J85-GE-5A turbojet engines engines 2 x Lycoming IO-540
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 400 lbs
4,100 pounds dry thrust; 5,800 with afterburners total thrust 800 lbs
12,093 lb 5,485 kg MTOW 8,500 lb 3,856 kg
1,759 km 950 nm range 850 nm 1,574 km
745 kts 1,380 km/h cruise speed 210 kts 130 mph
Two (student and instructor) capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.