Grumman OV-1 Mohawk vs. Lockheed P-2 Neptune
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Grumman OV-1 Mohawk |
versus |
Lockheed P-2 Neptune |
12.52 m |
41 ft 1 in |
length |
30.17 m |
99 ft 0 in |
3.89 m |
12 ft 9 in |
height |
10.15 m |
33 ft 4 in |
14.63 m |
48 ft |
wingspan |
33.53 m |
110 ft |
2 x Lycoming T53 turboprop engines |
engines |
2 x Wright R-3350 radial engines |
Approximately 1,100 hp each |
thrust per engine |
Approximately 3,700 hp |
Approximately 2,200 hp total |
total thrust |
Approximately 7,400 hp |
14,950 lb |
6,781 kg |
MTOW |
27,216 kg |
60,000 lb |
1,690 km |
913 nm |
range |
7,885 km |
4,259 nm |
230 mph |
370 km/h |
cruise speed |
300 mph |
483 km/h |
Pilot and observer |
capacity |
based on configuration |
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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.