McDonnell Douglas F-4 Phantom II vs. Northrop T-38 Talon

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McDonnell Douglas F-4 Phantom II versus Northrop T-38 Talon
19.2 m 63 ft 0 in length 14.1 m 46 ft 4 in
5.03 m 16 ft 6 in height 3.9 m 12 ft 10 in
11.72 m 38 ft 5 in wingspan 7.7 m 25 ft 3 in
Two General Electric J79s engines Two General Electric J85-GE-5A turbojet engines
17,900 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
35,800 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
27,965 kg 61,700 lb MTOW 12,093 lb 5,485 kg
3,031 km 1,636 nm range 1,759 km 950 nm
Mach 2.2 2,717 km/h cruise speed 745 kts 1,380 km/h
Up to 16,000 lbs of externally carried ordnance 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.