Mitsubishi A6M Zero vs. Northrop T-38 Talon

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Mitsubishi A6M Zero versus Northrop T-38 Talon
9.06 m 29 ft 9 in length 14.1 m 46 ft 4 in
3.05 m 10 ft height 3.9 m 12 ft 10 in
12 m 39 ft 4 in wingspan 7.7 m 25 ft 3 in
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine engines Two General Electric J85-GE-5A turbojet engines
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) total thrust 4,100 pounds dry thrust; 5,800 with afterburners
2,800 kg 6,170 lb MTOW 12,093 lb 5,485 kg
1,010 nm 1,871 km range 1,759 km 950 nm
180 knots 105 mph 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.