Cessna O-2 Skymaster vs. Northrop T-38 Talon
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Cessna O-2 Skymaster |
versus |
Northrop T-38 Talon |
8.9 m |
29 ft 2 in |
length |
14.1 m |
46 ft 4 in |
2.87 m |
9 ft 5 in |
height |
3.9 m |
12 ft 10 in |
11.58 m |
38 ft |
wingspan |
7.7 m |
25 ft 3 in |
Two 210-hp Continental IO-360s |
engines |
Two General Electric J85-GE-5A turbojet engines |
210 hp |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
420 hp |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
5,400 lb |
2,449 kg |
MTOW |
12,093 lb |
5,485 kg |
1,705 km |
921 nm |
range |
1,759 km |
950 nm |
144 mph |
232 km/h |
cruise speed |
745 kts |
1,380 km/h |
2 |
capacity |
Two (student and instructor) |
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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.