Northrop T-38 Talon vs. Lockheed C-69 Constellation

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Northrop T-38 Talon versus Lockheed C-69 Constellation
14.1 m 46 ft 4 in length 29.72 m 97 ft 6 in
3.9 m 12 ft 10 in height 6.02 m 19 ft 9 in
7.7 m 25 ft 3 in wingspan 37.49 m 123 ft
Two General Electric J85-GE-5A turbojet engines engines 4 x Wright R-3350 Duplex-Cyclone radial engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 8,800 to 14,800 horsepower
12,093 lb 5,485 kg MTOW 44,453 kg 98,000 lb
1,759 km 950 nm range 5,200 km 2,808 nm
745 kts 1,380 km/h cruise speed 507 km/h 315 mph
Two (student and instructor) capacity Up to 109 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.