Lockheed L-1011 TriStar 500 vs. Northrop T-38 Talon

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Lockheed L-1011 TriStar 500 versus Northrop T-38 Talon
50.05 m 164 ft 3 in length 14.1 m 46 ft 4 in
16.87 m 55 ft 4 in height 3.9 m 12 ft 10 in
50.09 m 164 ft 4 in wingspan 7.7 m 25 ft 3 in
3 Rolls-Royce RB211 engines engines Two General Electric J85-GE-5A turbojet engines
42,000 lbf thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
231,330 kg 510,000 lb MTOW 12,093 lb 5,485 kg
11,260 km 6,100 nm range 1,759 km 950 nm
525 knots 972 km/h cruise speed 745 kts 1,380 km/h
Max. 315 passengers (typical 253) 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.