Lockheed P-2 Neptune vs. Lockheed T-33 Shooting Star

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Lockheed P-2 Neptune versus Lockheed T-33 Shooting Star
30.17 m 99 ft 0 in length 11.51 m 37 ft 9 in
10.15 m 33 ft 4 in height 3.56 m 11 ft 8 in
33.53 m 110 ft wingspan 11.9 m 39 ft 1 in
2 x Wright R-3350 radial engines engines 1 (Allison J33-A-5)
Approximately 3,700 hp thrust per engine 24.0 kN
Approximately 7,400 hp total thrust 24.0 kN
27,216 kg 60,000 lb MTOW 5,900 kg 13,000 lb
7,885 km 4,259 nm range 2,050 km 1,107 nm
300 mph 483 km/h cruise speed 965 km/h 600 mph
based on configuration capacity 907 kg of bombs or rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.