Northrop T-38 Talon vs. Antonov An-124 Ruslan

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Northrop T-38 Talon versus Antonov An-124 Ruslan
14.1 m 46 ft 4 in length 69.10 m 226 ft 9 in
3.9 m 12 ft 10 in height 20.78 m 68 ft 2 in
7.7 m 25 ft 3 in wingspan 73.3 m 240 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 4 x Ivchenko Progress D-18T turbofan engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 51,590 lbf
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 206,360 lbf
12,093 lb 5,485 kg MTOW 405,000 kg 893,000 lb
1,759 km 950 nm range 3,700 km 1,998 nm
745 kts 1,380 km/h cruise speed 800 km/h 497 mph
Two (student and instructor) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.