Auster AOP.9 vs. Northrop T-38 Talon

versus
... or view the full comparison list here.
Auster AOP.9 versus Northrop T-38 Talon
7.23 m 23 ft 9 in length 14.1 m 46 ft 4 in
2.72 m 8 ft 11 in height 3.9 m 12 ft 10 in
11.1 m 36 ft 5 in wingspan 7.7 m 25 ft 3 in
1 x Blackburn Cirrus Bombardier 203 engines Two General Electric J85-GE-5A turbojet engines
134 kW (180 hp) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
134 kW (180 hp) (As it has only one engine) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
966 kg 2,130 lb MTOW 12,093 lb 5,485 kg
628 km 339 nm range 1,759 km 950 nm
177 km/h 110 mph cruise speed 745 kts 1,380 km/h
3 (pilot and two passengers) 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.