Northrop T-38 Talon vs. Aero Commander 690

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Northrop T-38 Talon versus Aero Commander 690
14.1 m 46 ft 4 in length 12.04 m 39 ft 6 in
3.9 m 12 ft 10 in height 3.75 m 12 ft 4 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 8,000 lb 3,629 kg
1,759 km 950 nm range 1,600 nm 2,963 km
745 kts 1,380 km/h cruise speed 260 kts 162 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.