Northrop T-38 Talon vs. Mil Mi-26

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Northrop T-38 Talon versus Mil Mi-26
14.1 m 46 ft 4 in length 40.03 m 131.3 ft
3.9 m 12 ft 10 in height 8.15 m 26.7 ft
7.7 m 25 ft 3 in wingspan
Two General Electric J85-GE-5A turbojet engines engines 2 x Lotarev D-136 turboshaft engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 8,380 kW
4,100 pounds dry thrust; 5,800 with afterburners total thrust 16,760 kW
12,093 lb 5,485 kg MTOW 56,000 kg 123,459 lb
1,759 km 950 nm range 800 km 432 nm
745 kts 1,380 km/h cruise speed 255 km/h 158 mph
Two (student and instructor) capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.