McDonnell Douglas F-4 Phantom II vs. Canadair CL-415

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McDonnell Douglas F-4 Phantom II versus Canadair CL-415
19.2 m 63 ft 0 in length 19.82 m 65 ft 0 in
5.03 m 16 ft 6 in height 8.66 m 28 ft 5 in
11.72 m 38 ft 5 in wingspan 28.6 m 93 ft 1
Two General Electric J79s engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
17,900 lbs thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
35,800 lbs total thrust 4,300 to 4,760 shaft horsepower
27,965 kg 61,700 lb MTOW 19,733 kg 43,525 lb
3,031 km 1,636 nm range 1,600 km 864 nm
Mach 2.2 2,717 km/h cruise speed 290 km/h 180 mph
Up to 16,000 lbs of externally carried ordnance capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.