North American P-51 Mustang vs. Northrop T-38 Talon

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North American P-51 Mustang versus Northrop T-38 Talon
9.83 m 32 ft 3 in length 14.1 m 46 ft 4 in
4.08 m 13 ft 5 in height 3.9 m 12 ft 10 in
11.28 m 37 ft wingspan 7.7 m 25 ft 3 in
Packard Rolls Royce Merlin V-1650-7 engines Two General Electric J85-GE-5A turbojet engines
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
5,489 kg 12,100 lb MTOW 12,093 lb 5,485 kg
2,200 km 1,188 nm range 1,759 km 950 nm
325 mph 525 km/h cruise speed 745 kts 1,380 km/h
2,000 pounds of bombs, or ten 5-inch rockets 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.