de Havilland Canada DHC-2 Beaver vs. McDonnell Douglas F-4 Phantom II

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de Havilland Canada DHC-2 Beaver versus McDonnell Douglas F-4 Phantom II
13.56 m 44 ft 6 in length 19.2 m 63 ft 0 in
5 m 16 ft 5 in height 5.03 m 16 ft 6 in
16.56 m 54 ft 4 in wingspan 11.72 m 38 ft 5 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines Two General Electric J79s
Approximately 3,100 hp (2,312 kW) each thrust per engine 17,900 lbs
Approximately 6,200 hp (4,624 kW) total total thrust 35,800 lbs
24,200 lb 10,977 kg MTOW 27,965 kg 61,700 lb
2,535 km 1,369 nm range 3,031 km 1,636 nm
228 mph 367 km/h cruise speed Mach 2.2 2,717 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.