Douglas DC-8-61 vs. Northrop T-38 Talon

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Douglas DC-8-61 versus Northrop T-38 Talon
57.0 m 187 ft 0 in length 14.1 m 46 ft 4 in
13.1 m 43 ft height 3.9 m 12 ft 10 in
45.24 m 148 ft 5 in wingspan 7.7 m 25 ft 3 in
4x P&W JT3D-3B Turbofan engines Two General Electric J85-GE-5A turbojet engines
18,000 pound-force thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
72,000 pound-force total thrust 4,100 pounds dry thrust; 5,800 with afterburners
147,400 kg 325,000 lb MTOW 12,093 lb 5,485 kg
3,200 nm 5,926 km range 1,759 km 950 nm
483 knots 282 mph cruise speed 745 kts 1,380 km/h
180 to 220 passengers in a mixed-class seating 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.