McDonnell Douglas F-4 Phantom II vs. North American F-100 Super Sabre
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| McDonnell Douglas F-4 Phantom II |
versus |
North American F-100 Super Sabre |
| 19.2 m |
63 ft 0 in |
length |
16.46 m |
54 ft 2 in |
| 5.03 m |
16 ft 6 in |
height |
4.93 m |
16 ft 2 in |
| 11.72 m |
38 ft 5 in |
wingspan |
11.84 m |
38 ft 1 |
| Two General Electric J79s |
engines |
1 Pratt & Whitney J57-P-21A |
| 17,900 lbs |
thrust per engine |
16,000 lb. thrust in afterburner |
| 35,800 lbs |
total thrust |
16,000 lb. (afterburner) |
| 27,965 kg |
61,700 lb |
MTOW |
17,609 kg |
38,800 lb |
| 3,031 km |
1,636 nm |
range |
2,673 km |
1,444 nm |
| Mach 2.2 |
2,717 km/h |
cruise speed |
587 mph |
945 km/h |
| Up to 16,000 lbs of externally carried ordnance |
capacity |
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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.
