Northrop T-38 Talon vs. Lockheed Martin C-130J Super Hercules

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Northrop T-38 Talon versus Lockheed Martin C-130J Super Hercules
14.1 m 46 ft 4 in length 34.37 m 112 ft 9 in
3.9 m 12 ft 10 in height 11.86 m 38 ft 11 in
7.7 m 25 ft 3 in wingspan 40.41 m 132 ft 7 in
Two General Electric J85-GE-5A turbojet engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 4,700 hp per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 18,800 hp total
12,093 lb 5,485 kg MTOW 76,610 kg 168,900 lb
1,759 km 950 nm range 4,600 km 2,485 nm
745 kts 1,380 km/h cruise speed 660 km/h 410 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.