McDonnell Douglas F-4 Phantom II vs. Short C-23 Sherpa

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McDonnell Douglas F-4 Phantom II versus Short C-23 Sherpa
19.2 m 63 ft 0 in length 17.68 m 58 ft 0 in
5.03 m 16 ft 6 in height 6.55 m 21 ft 6 in
11.72 m 38 ft 5 in wingspan 22.76 m 74 ft 8 in
Two General Electric J79s engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
17,900 lbs thrust per engine Approximately 1,200 hp per engine
35,800 lbs total thrust Approximately 2,400 hp total
27,965 kg 61,700 lb MTOW 7,484 kg 16,500 lb
3,031 km 1,636 nm range 1,048 km 566 nm
Mach 2.2 2,717 km/h cruise speed 425 km/h 264 mph
Up to 16,000 lbs of externally carried ordnance 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.