Grumman OV-1 Mohawk vs. Lockheed P-2 Neptune

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Grumman OV-1 Mohawk versus Lockheed P-2 Neptune
12.52 m 41 ft 1 in length 30.17 m 99 ft 0 in
3.89 m 12 ft 9 in height 10.15 m 33 ft 4 in
14.63 m 48 ft wingspan 33.53 m 110 ft
2 x Lycoming T53 turboprop engines engines 2 x Wright R-3350 radial engines
Approximately 1,100 hp each thrust per engine Approximately 3,700 hp
Approximately 2,200 hp total total thrust Approximately 7,400 hp
14,950 lb 6,781 kg MTOW 27,216 kg 60,000 lb
1,690 km 913 nm range 7,885 km 4,259 nm
230 mph 370 km/h cruise speed 300 mph 483 km/h
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.