Northrop T-38 Talon vs. Bell 412

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Northrop T-38 Talon versus Bell 412
14.1 m 46 ft 4 in length 17,10 m 56 ft 1 in
3.9 m 12 ft 10 in height 3,48 m 11 ft 5 in
7.7 m 25 ft 3 in wingspan
Two General Electric J85-GE-5A turbojet engines engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 1,800 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust 3,600 hp
12,093 lb 5,485 kg MTOW 5,400 kg 11,905 lb
1,759 km 950 nm range 659 km 356 nm
745 kts 1,380 km/h cruise speed 259 km/h 161 mph
Two (student and instructor) capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.