Lockheed P-2 Neptune vs. Northrop T-38 Talon

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Lockheed P-2 Neptune versus Northrop T-38 Talon
30.17 m 99 ft 0 in length 14.1 m 46 ft 4 in
10.15 m 33 ft 4 in height 3.9 m 12 ft 10 in
33.53 m 110 ft wingspan 7.7 m 25 ft 3 in
2 x Wright R-3350 radial engines engines Two General Electric J85-GE-5A turbojet engines
Approximately 3,700 hp thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
Approximately 7,400 hp total thrust 4,100 pounds dry thrust; 5,800 with afterburners
27,216 kg 60,000 lb MTOW 12,093 lb 5,485 kg
7,885 km 4,259 nm range 1,759 km 950 nm
300 mph 483 km/h cruise speed 745 kts 1,380 km/h
based on configuration 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.