Grumman OV-1 Mohawk vs. Lockheed Martin C-130J Super Hercules

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Grumman OV-1 Mohawk versus Lockheed Martin C-130J Super Hercules
12.52 m 41 ft 1 in length 34.37 m 112 ft 9 in
3.89 m 12 ft 9 in height 11.86 m 38 ft 11 in
14.63 m 48 ft wingspan 40.41 m 132 ft 7 in
2 x Lycoming T53 turboprop engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 1,100 hp each thrust per engine Approximately 4,700 hp per engine
Approximately 2,200 hp total total thrust Approximately 18,800 hp total
14,950 lb 6,781 kg MTOW 76,610 kg 168,900 lb
1,690 km 913 nm range 4,600 km 2,485 nm
230 mph 370 km/h cruise speed 660 km/h 410 mph
Pilot and observer capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.