Cessna O-2 Skymaster vs. McDonnell Douglas F-4 Phantom II
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Cessna O-2 Skymaster |
versus |
McDonnell Douglas F-4 Phantom II |
8.9 m |
29 ft 2 in |
length |
19.2 m |
63 ft 0 in |
2.87 m |
9 ft 5 in |
height |
5.03 m |
16 ft 6 in |
11.58 m |
38 ft |
wingspan |
11.72 m |
38 ft 5 in |
Two 210-hp Continental IO-360s |
engines |
Two General Electric J79s |
210 hp |
thrust per engine |
17,900 lbs |
420 hp |
total thrust |
35,800 lbs |
5,400 lb |
2,449 kg |
MTOW |
27,965 kg |
61,700 lb |
1,705 km |
921 nm |
range |
3,031 km |
1,636 nm |
144 mph |
232 km/h |
cruise speed |
Mach 2.2 |
2,717 km/h |
2 |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.