de Havilland Venom vs. Northrop T-38 Talon

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de Havilland Venom versus Northrop T-38 Talon
6.71 m 22 ft 0 in length 14.1 m 46 ft 4 in
1.88 m 6 ft 2 in height 3.9 m 12 ft 10 in
12.7 m 41 ft 8 in wingspan 7.7 m 25 ft 3 in
1 (de Havilland Ghost 105) engines Two General Electric J85-GE-5A turbojet engines
23.6 kN thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
23.6 kN total thrust 4,100 pounds dry thrust; 5,800 with afterburners
6,945 kg 15,300 lb MTOW 12,093 lb 5,485 kg
1,730 km 935 nm range 1,759 km 950 nm
1030 km/h 640 mph cruise speed 745 kts 1,380 km/h
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.