Cessna O-2 Skymaster vs. Northrop T-38 Talon

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Cessna O-2 Skymaster versus Northrop T-38 Talon
8.9 m 29 ft 2 in length 14.1 m 46 ft 4 in
2.87 m 9 ft 5 in height 3.9 m 12 ft 10 in
11.58 m 38 ft wingspan 7.7 m 25 ft 3 in
Two 210-hp Continental IO-360s engines Two General Electric J85-GE-5A turbojet engines
210 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
420 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
5,400 lb 2,449 kg MTOW 12,093 lb 5,485 kg
1,705 km 921 nm range 1,759 km 950 nm
144 mph 232 km/h cruise speed 745 kts 1,380 km/h
2 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.