Northrop T-38 Talon vs. Westland Lysander

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Northrop T-38 Talon versus Westland Lysander
14.1 m 46 ft 4 in length 9.3 m 30 ft 6 in
3.9 m 12 ft 10 in height 3.51 m 11 ft 6 in
7.7 m 25 ft 3 in wingspan 15.24 m 50 ft
Two General Electric J85-GE-5A turbojet engines engines 1 x Bristol Mercury XII radial engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 870 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 870 hp
12,093 lb 5,485 kg MTOW 7,500 lb 3,402 kg
1,759 km 950 nm range 966 km 522 nm
745 kts 1,380 km/h cruise speed 190 mph 306 km/h
Two (student and instructor) capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.