McDonnell-Douglas MD-11 vs. Northrop T-38 Talon

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McDonnell-Douglas MD-11 versus Northrop T-38 Talon
61.20 m 200 ft 10 in length 14.1 m 46 ft 4 in
17.6 m 57 ft 9 in height 3.9 m 12 ft 10 in
51.6 m 169 ft 4 in wingspan 7.7 m 25 ft 3 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines Two General Electric J85-GE-5A turbojet engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
285,990 kg 630,400 lb MTOW 12,093 lb 5,485 kg
13,231 km 7,147 nm range 1,759 km 950 nm
961 km/h 597 mph cruise speed 745 kts 1,380 km/h
Max 410 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.