Boeing 767-300ER vs. Northrop T-38 Talon

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Boeing 767-300ER versus Northrop T-38 Talon
54.9 m 180 ft 3 in length 14.1 m 46 ft 4 in
15.85 m 52 ft height 3.9 m 12 ft 10 in
47.57 m 156 ft 1 in wingspan 7.7 m 25 ft 3 in
Two Pratt & Whitney PW4060 turbofan engines engines Two General Electric J85-GE-5A turbojet engines
Up to 63,300 pounds of thrust each thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Up to 126,600 pounds of thrust total thrust 4,100 pounds dry thrust; 5,800 with afterburners
186,880 kg 412,000 lb MTOW 12,093 lb 5,485 kg
11,070 km 5,980 nm range 1,759 km 950 nm
528 MPH 850 km/h cruise speed 745 kts 1,380 km/h
Typically 218 (3-class) 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.