Cessna O-2 Skymaster vs. North American P-51 Mustang
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Cessna O-2 Skymaster |
versus |
North American P-51 Mustang |
8.9 m |
29 ft 2 in |
length |
9.83 m |
32 ft 3 in |
2.87 m |
9 ft 5 in |
height |
4.08 m |
13 ft 5 in |
11.58 m |
38 ft |
wingspan |
11.28 m |
37 ft |
Two 210-hp Continental IO-360s |
engines |
Packard Rolls Royce Merlin V-1650-7 |
210 hp |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
420 hp |
total thrust |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
5,400 lb |
2,449 kg |
MTOW |
5,489 kg |
12,100 lb |
1,705 km |
921 nm |
range |
2,200 km |
1,188 nm |
144 mph |
232 km/h |
cruise speed |
325 mph |
525 km/h |
2 |
capacity |
2,000 pounds of bombs, or ten 5-inch rockets |
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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.