Lockheed SR-71 Blackbird vs. Northrop T-38 Talon

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Lockheed SR-71 Blackbird versus Northrop T-38 Talon
32.74 m 107 ft 5 in length 14.1 m 46 ft 4 in
5.64 m 18 ft 6 in height 3.9 m 12 ft 10 in
16.94 m 55 ft 7 in wingspan 7.7 m 25 ft 3 in
Two Pratt & Whitney J58 axial-flow turbojets engines Two General Electric J85-GE-5A turbojet engines
34,000 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
68,000 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
78,018 kg 172,000 lb MTOW 12,093 lb 5,485 kg
3,250 mi 2,832 nm range 1,759 km 950 nm
Mach 3.2 3951 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.