Max Holste M.H.1521 Broussard vs. Northrop T-38 Talon

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Max Holste M.H.1521 Broussard versus Northrop T-38 Talon
10.46 m 34 ft 4 in length 14.1 m 46 ft 4 in
2.74 m 9 ft height 3.9 m 12 ft 10 in
12.86 m 42 ft 2 in wingspan 7.7 m 25 ft 3 in
1 x Lycoming GSO-480-B1A6 flat-six engine engines Two General Electric J85-GE-5A turbojet engines
Approximately 295 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 295 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
1,900 kg 4,189 lb MTOW 12,093 lb 5,485 kg
1,030 km 556 nm range 1,759 km 950 nm
145 mph 233 km/h cruise speed 745 kts 1,380 km/h
5-7 passengers 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.