Aermacchi MB-326 vs. Northrop T-38 Talon

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Aermacchi MB-326 versus Northrop T-38 Talon
10.67 m 35 ft 0 in length 14.1 m 46 ft 4 in
3.71 m 12 ft 2 in height 3.9 m 12 ft 10 in
10.82 m 35 ft 6 in wingspan 7.7 m 25 ft 3 in
1 x Rolls-Royce “Viper” 632-42 turbojet engines Two General Electric J85-GE-5A turbojet engines
4,000 lb thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
4,000 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
5,897 kg 13,000 lb MTOW 12,093 lb 5,485 kg
677 mi 589 nm range 1,759 km 950 nm
553 mph 890 km/h 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.