McDonnell-Douglas DC-9-30 vs. Northrop T-38 Talon

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McDonnell-Douglas DC-9-30 versus Northrop T-38 Talon
36.36 m 119 ft 3 in length 14.1 m 46 ft 4 in
8.5 m 27 ft 11 in height 3.9 m 12 ft 10 in
28.44 m 93 ft 4 in wingspan 7.7 m 25 ft 3 in
2x Pratt & Whitney JT8D engines Two General Electric J85-GE-5A turbojet engines
15,000 pound-force thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
30,000 pound-force (2 engines) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
54,885 kg 121,000 lb MTOW 12,093 lb 5,485 kg
2,632 km 1,422 nm range 1,759 km 950 nm
898 km/h 558 mph cruise speed 745 kts 1,380 km/h
Up to 139 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.