Northrop T-38 Talon vs. Dornier 228

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Northrop T-38 Talon versus Dornier 228
14.1 m 46 ft 4 in length 16.56 m 54 ft 4 in
3.9 m 12 ft 10 in height 4.86 m 15 ft 11 in
7.7 m 25 ft 3 in wingspan 16.97 m 55 ft 8 in
Two General Electric J85-GE-5A turbojet engines engines 2 x Garrett TPE331 turboprop engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 776 kW per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 1,552 kW total
12,093 lb 5,485 kg MTOW 5,650 kg 12,456 lb
1,759 km 950 nm range 1,465 km 791 nm
745 kts 1,380 km/h cruise speed 350 km/h 217 mph
Two (student and instructor) capacity Up to 19 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.