Northrop T-38 Talon vs. Douglas DC-6

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Northrop T-38 Talon versus Douglas DC-6
14.1 m 46 ft 4 in length 32.18 m 105 ft 7 in
3.9 m 12 ft 10 in height 8.94 m 29 ft 4 in
7.7 m 25 ft 3 in wingspan 35.81 m 117 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 4 x Pratt & Whitney R-2800-CB17 radial engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 2,500 hp per engine
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 10,000 hp total
12,093 lb 5,485 kg MTOW 52,200 kg 115,100 lb
1,759 km 950 nm range 5,800 km 3,133 nm
745 kts 1,380 km/h cruise speed 507 km/h 315 mph
Two (student and instructor) capacity Up to 102 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.