Grumman OV-1 Mohawk vs. McDonnell Douglas F-4 Phantom II

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Grumman OV-1 Mohawk versus McDonnell Douglas F-4 Phantom II
12.52 m 41 ft 1 in length 19.2 m 63 ft 0 in
3.89 m 12 ft 9 in height 5.03 m 16 ft 6 in
14.63 m 48 ft wingspan 11.72 m 38 ft 5 in
2 x Lycoming T53 turboprop engines engines Two General Electric J79s
Approximately 1,100 hp each thrust per engine 17,900 lbs
Approximately 2,200 hp total total thrust 35,800 lbs
14,950 lb 6,781 kg MTOW 27,965 kg 61,700 lb
1,690 km 913 nm range 3,031 km 1,636 nm
230 mph 370 km/h cruise speed Mach 2.2 2,717 km/h
Pilot and observer capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.