Northrop T-38 Talon vs. Aero Commander 680

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Northrop T-38 Talon versus Aero Commander 680
14.1 m 46 ft 4 in length 11.38 m 37 ft 4 in
3.9 m 12 ft 10 in height 3.6 m 11 ft 10 in
7.7 m 25 ft 3 in wingspan 15.02 m 49 ft 3 in
Two General Electric J85-GE-5A turbojet engines engines 2 x Lycoming TIO-540
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 380 lbs
4,100 pounds dry thrust; 5,800 with afterburners total thrust 760 lbs
12,093 lb 5,485 kg MTOW 7,500 lb 3,402 kg
1,759 km 950 nm range 1,500 nm 2,778 km
745 kts 1,380 km/h cruise speed 218 kts 135 mph
Two (student and instructor) capacity Up to 6 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.