Lockheed P-2 Neptune vs. McDonnell Douglas F-4 Phantom II

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Lockheed P-2 Neptune versus McDonnell Douglas F-4 Phantom II
30.17 m 99 ft 0 in length 19.2 m 63 ft 0 in
10.15 m 33 ft 4 in height 5.03 m 16 ft 6 in
33.53 m 110 ft wingspan 11.72 m 38 ft 5 in
2 x Wright R-3350 radial engines engines Two General Electric J79s
Approximately 3,700 hp thrust per engine 17,900 lbs
Approximately 7,400 hp total thrust 35,800 lbs
27,216 kg 60,000 lb MTOW 27,965 kg 61,700 lb
7,885 km 4,259 nm range 3,031 km 1,636 nm
300 mph 483 km/h cruise speed Mach 2.2 2,717 km/h
based on configuration capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.