McDonnell Douglas F-4 Phantom II vs. Aero Commander 560
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McDonnell Douglas F-4 Phantom II |
versus |
Aero Commander 560 |
19.2 m |
63 ft 0 in |
length |
10.88 m |
35 ft 8 in |
5.03 m |
16 ft 6 in |
height |
3.6 m |
11 ft 10 in |
11.72 m |
38 ft 5 in |
wingspan |
15.02 m |
49 ft 3 in |
Two General Electric J79s |
engines |
2 x Lycoming TIO-540 |
17,900 lbs |
thrust per engine |
340 lbs |
35,800 lbs |
total thrust |
680 lbs |
27,965 kg |
61,700 lb |
MTOW |
6,000 lb |
2,722 kg |
3,031 km |
1,636 nm |
range |
1,200 nm |
2,222 km |
Mach 2.2 |
2,717 km/h |
cruise speed |
210 kts |
130 mph |
Up to 16,000 lbs of externally carried ordnance |
capacity |
Up to 6 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.