McDonnell Douglas F-4 Phantom II vs. Aero Commander 500S
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McDonnell Douglas F-4 Phantom II |
versus |
Aero Commander 500S |
19.2 m |
63 ft 0 in |
length |
10.46 m |
34 ft 4 in |
5.03 m |
16 ft 6 in |
height |
3.63 m |
11 ft 11 in |
11.72 m |
38 ft 5 in |
wingspan |
13.52 m |
44 ft 4 in |
Two General Electric J79s |
engines |
2 x Lycoming IO-540 |
17,900 lbs |
thrust per engine |
380 lbs |
35,800 lbs |
total thrust |
760 lbs |
27,965 kg |
61,700 lb |
MTOW |
11,500 lb |
5,216 kg |
3,031 km |
1,636 nm |
range |
1,350 nm |
2,500 km |
Mach 2.2 |
2,717 km/h |
cruise speed |
230 kts |
143 mph |
Up to 16,000 lbs of externally carried ordnance |
capacity |
Up to 4 passengers |
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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.