North American Rockwell OV-10 Bronco vs. Northrop T-38 Talon

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North American Rockwell OV-10 Bronco versus Northrop T-38 Talon
12.7 m 41 ft 7 in length 14.1 m 46 ft 4 in
4.62 m 15 ft 2 in height 3.9 m 12 ft 10 in
12.19 m 40 ft wingspan 7.7 m 25 ft 3 in
2 x Garrett T76-G-420/421 turboprop engines engines Two General Electric J85-GE-5A turbojet engines
Approximately 715 hp each thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 1,430 hp total total thrust 4,100 pounds dry thrust; 5,800 with afterburners
14,444 lb 6,553 kg MTOW 12,093 lb 5,485 kg
1,931 km 1,043 nm range 1,759 km 950 nm
244 mph 393 km/h cruise speed 745 kts 1,380 km/h
Pilot and observer 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.