Auster AOP.6 vs. Northrop T-38 Talon

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Auster AOP.6 versus Northrop T-38 Talon
7.24 m 23 ft 9 in length 14.1 m 46 ft 4 in
2.55 m 8 ft 4 in height 3.9 m 12 ft 10 in
10.97 m 36 ft wingspan 7.7 m 25 ft 3 in
1× de Havilland Gipsy Major 7 inline piston engines Two General Electric J85-GE-5A turbojet engines
145 hp (108 kW) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
145 hp (108 kW) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
2,160 lb 980 kg MTOW 12,093 lb 5,485 kg
507 km 274 nm range 1,759 km 950 nm
174 km/h 108 mph cruise speed 745 kts 1,380 km/h
capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.