Northrop T-38 Talon vs. Lockheed Model 18 Lodestar

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Northrop T-38 Talon versus Lockheed Model 18 Lodestar
14.1 m 46 ft 4 in length 13.61 m 44 ft 8 in
3.9 m 12 ft 10 in height 3.63 m 11 ft 11 in
7.7 m 25 ft 3 in wingspan 19.96 m 65 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 2 x Wright R-1820 Cyclone radial engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 1,200 to 1,350 horsepower (895 to 1,007 kW)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 2,400 to 2,700 horsepower
12,093 lb 5,485 kg MTOW 9,979 kg 22,000 lb
1,759 km 950 nm range 2,500 km 1,350 nm
745 kts 1,380 km/h cruise speed 300 km/h 186 mph
Two (student and instructor) capacity 14 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.