Grumman OV-1 Mohawk vs. Lockheed Martin F-35 Lightning II
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Grumman OV-1 Mohawk |
versus |
Lockheed Martin F-35 Lightning II |
12.52 m |
41 ft 1 in |
length |
15.67 m |
51 ft 4 in |
3.89 m |
12 ft 9 in |
height |
4.33 m |
14 ft 2 in |
14.63 m |
48 ft |
wingspan |
10.7 m |
35 ft 1 in |
2 x Lycoming T53 turboprop engines |
engines |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
Approximately 1,100 hp each |
thrust per engine |
40,000 lb |
Approximately 2,200 hp total |
total thrust |
40,000 lb |
14,950 lb |
6,781 kg |
MTOW |
31,800 kg |
70,000 lb |
1,690 km |
913 nm |
range |
1,380 mi |
1,200 nm |
230 mph |
370 km/h |
cruise speed |
520 kt |
302 mph |
Pilot and observer |
capacity |
18,000 pounds of total ordinance |
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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.