McDonnell Douglas F-4 Phantom II vs. de Havilland Canada DHC-3 Otter
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| McDonnell Douglas F-4 Phantom II |
versus |
de Havilland Canada DHC-3 Otter |
| 19.2 m |
63 ft 0 in |
length |
10.52 m |
34 ft 6 in |
| 5.03 m |
16 ft 6 in |
height |
3.84 m |
12 ft 7 in |
| 11.72 m |
38 ft 5 in |
wingspan |
17.68 m |
58 ft |
| Two General Electric J79s |
engines |
1 x Pratt & Whitney R-1340 radial engine |
| 17,900 lbs |
thrust per engine |
400 to 600 horsepower (298 to 447 kW) |
| 35,800 lbs |
total thrust |
400 to 600 horsepower (298 to 447 kW) |
| 27,965 kg |
61,700 lb |
MTOW |
5,670 kg |
12,500 lb |
| 3,031 km |
1,636 nm |
range |
1,296 km |
700 nm |
| Mach 2.2 |
2,717 km/h |
cruise speed |
215 km/h |
134 mph |
| Up to 16,000 lbs of externally carried ordnance |
capacity |
10-11 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.
