McDonnell Douglas F-4 Phantom II vs. Beechcraft King Air 360

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McDonnell Douglas F-4 Phantom II versus Beechcraft King Air 360
19.2 m 63 ft 0 in length 13.39 m 43 ft 11 in
5.03 m 16 ft 6 in height 4.35 m 14 ft 3 in
11.72 m 38 ft 5 in wingspan 17.38 m 57 ft 1 in
Two General Electric J79s engines 2 x Pratt & Whitney Canada PT6A turboprop
17,900 lbs thrust per engine 1050 lbs
35,800 lbs total thrust 2100 lbs
27,965 kg 61,700 lb MTOW 14,000 lb 6,350 kg
3,031 km 1,636 nm range 1,720 nm 3,185 km
Mach 2.2 2,717 km/h cruise speed 310 kts 193 mph
Up to 16,000 lbs of externally carried ordnance capacity 9
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.