Northrop T-38 Talon vs. Scottish Aviation T1 Bulldog

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Northrop T-38 Talon versus Scottish Aviation T1 Bulldog
14.1 m 46 ft 4 in length 7.11 m 23 ft 4 in
3.9 m 12 ft 10 in height 2.08 m 6 ft 10 in
7.7 m 25 ft 3 in wingspan 10.21 m 33 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 1 x Lycoming O-360-A4M piston engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine Approximately 180 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust Approximately 180 hp
12,093 lb 5,485 kg MTOW 1,111 kg 2,450 lb
1,759 km 950 nm range 1,050 km 567 nm
745 kts 1,380 km/h cruise speed 222 km/h 138 mph
Two (student and instructor) capacity Instructor pilot and one student
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.