McDonnell Douglas F-4 Phantom II vs. Cessna 172
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here.
| McDonnell Douglas F-4 Phantom II |
versus |
Cessna 172 |
| 19.2 m |
63 ft 0 in |
length |
8.28 m |
27 ft 2 in |
| 5.03 m |
16 ft 6 in |
height |
2.72 m |
8 ft 11 in |
| 11.72 m |
38 ft 5 in |
wingspan |
11 m |
36 ft 1 in |
| Two General Electric J79s |
engines |
1 x Lycoming IO-360-L2A flat-4 piston engine |
| 17,900 lbs |
thrust per engine |
180 to 200 horsepower (134 to 149 kW) |
| 35,800 lbs |
total thrust |
180 to 200 horsepower (134 to 149 kW) |
| 27,965 kg |
61,700 lb |
MTOW |
1,040 kg |
2,293 lb |
| 3,031 km |
1,636 nm |
range |
1,056 km |
570 nm |
| Mach 2.2 |
2,717 km/h |
cruise speed |
226 km/h |
140 mph |
| Up to 16,000 lbs of externally carried ordnance |
capacity |
4 |
|
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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.
