Concorde vs. Northrop T-38 Talon

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Concorde versus Northrop T-38 Talon
61.66 m 202 ft 4 in length 14.1 m 46 ft 4 in
11.4 m 37 ft 5 in height 3.9 m 12 ft 10 in
25.56 m 83 ft 1 wingspan 7.7 m 25 ft 3 in
4 Rolls Royce/Snecma Olympus 593 turbo jet engines engines Two General Electric J85-GE-5A turbojet engines
18.7 tons (180 kN) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
74.8 tons (720 kN) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
185,000 kg 408,000 lb MTOW 12,093 lb 5,485 kg
6,580 km 3,554 nm range 1,759 km 950 nm
Mach 2.04 2,179 km/h cruise speed 745 kts 1,380 km/h
92–120 passengers 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.