Northrop T-38 Talon vs. Piper PA-34 Seneca

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Northrop T-38 Talon versus Piper PA-34 Seneca
14.1 m 46 ft 4 in length 8.71 m 28 ft 7 in
3.9 m 12 ft 10 in height 2.99 m 9 ft 10 in
7.7 m 25 ft 3 in wingspan 11.64 m 38 ft 2 in
Two General Electric J85-GE-5A turbojet engines engines 2 x Continental IO-360
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 220 lbs
4,100 pounds dry thrust; 5,800 with afterburners total thrust 440 lbs
12,093 lb 5,485 kg MTOW 4,750 lb 2,155 kg
1,759 km 950 nm range 980 nm 1,815 km
745 kts 1,380 km/h cruise speed 165 kts 103 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.