Northrop T-38 Talon vs. lockheed C-130 hercules

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Northrop T-38 Talon versus lockheed C-130 hercules
14.1 m 46 ft 4 in length 29.79 m 97 ft 9 in
3.9 m 12 ft 10 in height 11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 4,590 hp per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 18,360 hp total
12,093 lb 5,485 kg MTOW 70,307 kg 155,000 lb
1,759 km 950 nm range 3,760 km 2,031 nm
745 kts 1,380 km/h cruise speed 540 km/h 335 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.