McDonnell Douglas F-4 Phantom II vs. North American Rockwell OV-10 Bronco

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McDonnell Douglas F-4 Phantom II versus North American Rockwell OV-10 Bronco
19.2 m 63 ft 0 in length 12.7 m 41 ft 7 in
5.03 m 16 ft 6 in height 4.62 m 15 ft 2 in
11.72 m 38 ft 5 in wingspan 12.19 m 40 ft
Two General Electric J79s engines 2 x Garrett T76-G-420/421 turboprop engines
17,900 lbs thrust per engine Approximately 715 hp each
35,800 lbs total thrust Approximately 1,430 hp total
27,965 kg 61,700 lb MTOW 14,444 lb 6,553 kg
3,031 km 1,636 nm range 1,931 km 1,043 nm
Mach 2.2 2,717 km/h cruise speed 244 mph 393 km/h
Up to 16,000 lbs of externally carried ordnance capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.