Boeing F/A-18E/F Super Hornet vs. Northrop T-38 Talon

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Boeing F/A-18E/F Super Hornet versus Northrop T-38 Talon
18.5 m 60 ft 3 in length 14.1 m 46 ft 4 in
4.87 m 16 ft height 3.9 m 12 ft 10 in
13.68 m 44 ft 1 wingspan 7.7 m 25 ft 3 in
Two F414-GE-400 turbofan engines engines Two General Electric J85-GE-5A turbojet engines
Up to 17,000 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Up to 34,000 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
29,937 kg 66,000 lb MTOW 12,093 lb 5,485 kg
2,346 km 1,268 nm range 1,759 km 950 nm
1032 knots 1,911 km/h cruise speed 745 kts 1,380 km/h
Overall capability across all eleven hardpoints is 17,750lbs of external stores capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.