Consolidated B-24 Liberator vs. Northrop T-38 Talon

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Consolidated B-24 Liberator versus Northrop T-38 Talon
20.42 m 67 ft 0 in length 14.1 m 46 ft 4 in
5.49 m 18 ft height 3.9 m 12 ft 10 in
33.53 m 110 ft wingspan 7.7 m 25 ft 3 in
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines engines Two General Electric J85-GE-5A turbojet engines
1,200 hp, 1,200 hp each thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
4,800 hp (calculated from 4 engines each with 1,200 hp) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
26,580 kg 58,600 lb MTOW 12,093 lb 5,485 kg
2,850 mi 2,481 nm range 1,759 km 950 nm
175 mph 282 km/h cruise speed 745 kts 1,380 km/h
8,000 pounds 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.