Northrop T-38 Talon vs. Antonov An-225 Mriya

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Northrop T-38 Talon versus Antonov An-225 Mriya
14.1 m 46 ft 4 in length 84.0 m 275 ft 7 in
3.9 m 12 ft 10 in height 18.1 m 59 ft 5 in
7.7 m 25 ft 3 in wingspan 88.4 m 290 ft 2 in
Two General Electric J85-GE-5A turbojet engines engines 6 x Ivchenko Progress D-18T turbofan engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 23,400 kgf per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 140,400 kgf total
12,093 lb 5,485 kg MTOW 640,000 kg 1,411,200 lb
1,759 km 950 nm range 15,400 km 8,315 nm
745 kts 1,380 km/h cruise speed 800 km/h 497 mph
Two (student and instructor) capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.