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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.