de Havilland Canada DHC-2 Beaver vs. Northrop T-38 Talon

versus
... or view the full comparison list here.
de Havilland Canada DHC-2 Beaver versus Northrop T-38 Talon
13.56 m 44 ft 6 in length 14.1 m 46 ft 4 in
5 m 16 ft 5 in height 3.9 m 12 ft 10 in
16.56 m 54 ft 4 in wingspan 7.7 m 25 ft 3 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines Two General Electric J85-GE-5A turbojet engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 6,200 hp (4,624 kW) total total thrust 4,100 pounds dry thrust; 5,800 with afterburners
24,200 lb 10,977 kg MTOW 12,093 lb 5,485 kg
2,535 km 1,369 nm range 1,759 km 950 nm
228 mph 367 km/h cruise speed 745 kts 1,380 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.