Northrop T-38 Talon vs. PZL TS-11 Iskra

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Northrop T-38 Talon versus PZL TS-11 Iskra
14.1 m 46 ft 4 in length 11.15 m 36 ft 7 in
3.9 m 12 ft 10 in height 3.5 m 11 ft 6 in
7.7 m 25 ft 3 in wingspan 10.06 m 33 ft
Two General Electric J85-GE-5A turbojet engines engines 1 (WSK PZL Rzeszow SO-3W)
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 10.8 kN
4,100 pounds dry thrust; 5,800 with afterburners total thrust 10.8 kN
12,093 lb 5,485 kg MTOW 3,840 kg 8,466 lb
1,759 km 950 nm range 1,250 km 675 nm
745 kts 1,380 km/h cruise speed 770 km/h 478 mph
Two (student and instructor) capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.