Grumman OV-1 Mohawk vs. Airbus A300-600F

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Grumman OV-1 Mohawk versus Airbus A300-600F
12.52 m 41 ft 1 in length 54.08 m 177 ft 5 in
3.89 m 12 ft 9 in height 17.05 m 55 ft 11 in
14.63 m 48 ft wingspan 44.84 m 147 ft 1 in
2 x Lycoming T53 turboprop engines engines 2 x General Electric CF6-80C2A5 turbofan engines
Approximately 1,100 hp each thrust per engine Approximately 59,000 lbf per engine
Approximately 2,200 hp total total thrust Approximately 118,000 lbf total
14,950 lb 6,781 kg MTOW 170,000 kg 374,786 lb
1,690 km 913 nm range 4,830 km 2,608 nm
230 mph 370 km/h cruise speed 860 km/h 534 mph
Pilot and observer capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.