de Havilland Canada DHC-2 Beaver vs. McDonnell Douglas A-4 Skyhawk

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de Havilland Canada DHC-2 Beaver versus McDonnell Douglas A-4 Skyhawk
13.56 m 44 ft 6 in length 12.19 m 40 ft 0 in
5 m 16 ft 5 in height 4.57 m 15 ft
16.56 m 54 ft 4 in wingspan 8.08 m 26 ft 6 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1x Pratt & Whitney J52-P-6A Jet
Approximately 3,100 hp (2,312 kW) each thrust per engine 8,500 pound-force
Approximately 6,200 hp (4,624 kW) total total thrust 8,500 pound-force
24,200 lb 10,977 kg MTOW 11,113 kg 24,500 lb
2,535 km 1,369 nm range 3,222 km 1,739 nm
228 mph 367 km/h cruise speed 586 kts 364 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity Up to 9,155 pounds of weapons on 5 hardpoints
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.