Grumman OV-1 Mohawk vs. Antonov An-225 Mriya

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Grumman OV-1 Mohawk versus Antonov An-225 Mriya
12.52 m 41 ft 1 in length 84.0 m 275 ft 7 in
3.89 m 12 ft 9 in height 18.1 m 59 ft 5 in
14.63 m 48 ft wingspan 88.4 m 290 ft 2 in
2 x Lycoming T53 turboprop engines engines 6 x Ivchenko Progress D-18T turbofan engines
Approximately 1,100 hp each thrust per engine Approximately 23,400 kgf per engine
Approximately 2,200 hp total total thrust Approximately 140,400 kgf total
14,950 lb 6,781 kg MTOW 640,000 kg 1,411,200 lb
1,690 km 913 nm range 15,400 km 8,315 nm
230 mph 370 km/h cruise speed 800 km/h 497 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.