Boeing 747-400 vs. Northrop T-38 Talon

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Boeing 747-400 versus Northrop T-38 Talon
70.56 m 231 ft 10 in length 14.1 m 46 ft 4 in
19.3 m 63 ft 4 in height 3.9 m 12 ft 10 in
59.49 m 195 ft 4 in wingspan 7.7 m 25 ft 3 in
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H engines Two General Electric J85-GE-5A turbojet engines
Around 60,000 to 70,000 pounds thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Around 240,000 to 280,000 pounds total thrust 4,100 pounds dry thrust; 5,800 with afterburners
396,834 kg 875,000 lb MTOW 12,093 lb 5,485 kg
13,492 km 7,285 nmi range 1,759 km 950 nm
939 km/h 584 mph cruise speed 745 kts 1,380 km/h
Typically accommodates 416 passengers in a three-class layout 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.