Grumman OV-1 Mohawk vs. Northrop T-38 Talon
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Grumman OV-1 Mohawk |
versus |
Northrop T-38 Talon |
12.52 m |
41 ft 1 in |
length |
14.1 m |
46 ft 4 in |
3.89 m |
12 ft 9 in |
height |
3.9 m |
12 ft 10 in |
14.63 m |
48 ft |
wingspan |
7.7 m |
25 ft 3 in |
2 x Lycoming T53 turboprop engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
Approximately 1,100 hp each |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
Approximately 2,200 hp total |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
14,950 lb |
6,781 kg |
MTOW |
12,093 lb |
5,485 kg |
1,690 km |
913 nm |
range |
1,759 km |
950 nm |
230 mph |
370 km/h |
cruise speed |
745 kts |
1,380 km/h |
Pilot and observer |
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.