Northrop T-38 Talon vs. Cessna 152

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Northrop T-38 Talon versus Cessna 152
14.1 m 46 ft 4 in length 7.34 m 24 ft 1 in
3.9 m 12 ft 10 in height 2.59 m 8 ft 6 in
7.7 m 25 ft 3 in wingspan 10.16 m 33 ft 4 in
Two General Electric J85-GE-5A turbojet engines engines 1 x Lycoming O-235-L2C flat-4 piston engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 115 horsepower (86 kW)
4,100 pounds dry thrust; 5,800 with afterburners total thrust 115 horsepower (86 kW)
12,093 lb 5,485 kg MTOW 757 kg 1,669 lb
1,759 km 950 nm range 610 km 329 nm
745 kts 1,380 km/h cruise speed 185 km/h 115 mph
Two (student and instructor) capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.