McDonnell Douglas F-4 Phantom II vs. lockheed C-130 hercules
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McDonnell Douglas F-4 Phantom II |
versus |
lockheed C-130 hercules |
19.2 m |
63 ft 0 in |
length |
29.79 m |
97 ft 9 in |
5.03 m |
16 ft 6 in |
height |
11.66 m |
38 ft 3 in |
11.72 m |
38 ft 5 in |
wingspan |
40.41 m |
132 ft 7 in |
Two General Electric J79s |
engines |
4 x Allison T56-A-15 turboprop engines |
17,900 lbs |
thrust per engine |
Approximately 4,590 hp per engine |
35,800 lbs |
total thrust |
Approximately 18,360 hp total |
27,965 kg |
61,700 lb |
MTOW |
70,307 kg |
155,000 lb |
3,031 km |
1,636 nm |
range |
3,760 km |
2,031 nm |
Mach 2.2 |
2,717 km/h |
cruise speed |
540 km/h |
335 mph |
Up to 16,000 lbs of externally carried ordnance |
capacity |
based on configuration |
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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.