Grumman OV-1 Mohawk vs. Lockheed U-2
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Grumman OV-1 Mohawk |
versus |
Lockheed U-2 |
12.52 m |
41 ft 1 in |
length |
19.2 m |
63 ft 0 in |
3.89 m |
12 ft 9 in |
height |
4.8 m |
15 ft 9 in |
14.63 m |
48 ft |
wingspan |
32 m |
105 ft |
2 x Lycoming T53 turboprop engines |
engines |
1 × General Electric F118-101 |
Approximately 1,100 hp each |
thrust per engine |
17,000 lbf (76 kN) |
Approximately 2,200 hp total |
total thrust |
17,000 lbf (76 kN) |
14,950 lb |
6,781 kg |
MTOW |
18,144 kg |
40,000 lb |
1,690 km |
913 nm |
range |
6,090 nm |
11,278 km |
230 mph |
370 km/h |
cruise speed |
475 mph |
764 km/h |
Pilot and observer |
capacity |
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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.