Grumman OV-1 Mohawk vs. lockheed C-130 hercules

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Grumman OV-1 Mohawk versus lockheed C-130 hercules
12.52 m 41 ft 1 in length 29.79 m 97 ft 9 in
3.89 m 12 ft 9 in height 11.66 m 38 ft 3 in
14.63 m 48 ft wingspan 40.41 m 132 ft 7 in
2 x Lycoming T53 turboprop engines engines 4 x Allison T56-A-15 turboprop engines
Approximately 1,100 hp each thrust per engine Approximately 4,590 hp per engine
Approximately 2,200 hp total total thrust Approximately 18,360 hp total
14,950 lb 6,781 kg MTOW 70,307 kg 155,000 lb
1,690 km 913 nm range 3,760 km 2,031 nm
230 mph 370 km/h cruise speed 540 km/h 335 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.