Lockheed Martin F-35 Lightning II vs. McDonnell Douglas F-4 Phantom II
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Lockheed Martin F-35 Lightning II |
versus |
McDonnell Douglas F-4 Phantom II |
15.67 m |
51 ft 4 in |
length |
19.2 m |
63 ft 0 in |
4.33 m |
14 ft 2 in |
height |
5.03 m |
16 ft 6 in |
10.7 m |
35 ft 1 in |
wingspan |
11.72 m |
38 ft 5 in |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
Two General Electric J79s |
40,000 lb |
thrust per engine |
17,900 lbs |
40,000 lb |
total thrust |
35,800 lbs |
31,800 kg |
70,000 lb |
MTOW |
27,965 kg |
61,700 lb |
1,380 mi |
1,200 nm |
range |
3,031 km |
1,636 nm |
520 kt |
302 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
18,000 pounds of total ordinance |
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.