CASA 2.111 vs. Northrop T-38 Talon

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CASA 2.111 versus Northrop T-38 Talon
16.4 m 53 ft 10 in length 14.1 m 46 ft 4 in
3.9 m 12 ft 10 in height 3.9 m 12 ft 10 in
22.5 m 73 ft 1 wingspan 7.7 m 25 ft 3 in
2 × Rolls-Royce Merlin 500-29 V-12 liquid-cooled piston engines engines Two General Electric J85-GE-5A turbojet engines
1,176 kW (1,577 hp) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
2,352 kW (3,154 hp) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
14,000 kg 30,900 lb MTOW 12,093 lb 5,485 kg
1,950 km 1,053 nm range 1,759 km 950 nm
315 km/h 196 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.