de Havilland Canada DHC-2 Beaver vs. Lockheed Martin F-35 Lightning II

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de Havilland Canada DHC-2 Beaver versus Lockheed Martin F-35 Lightning II
13.56 m 44 ft 6 in length 15.67 m 51 ft 4 in
5 m 16 ft 5 in height 4.33 m 14 ft 2 in
16.56 m 54 ft 4 in wingspan 10.7 m 35 ft 1 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
Approximately 3,100 hp (2,312 kW) each thrust per engine 40,000 lb
Approximately 6,200 hp (4,624 kW) total total thrust 40,000 lb
24,200 lb 10,977 kg MTOW 31,800 kg 70,000 lb
2,535 km 1,369 nm range 1,380 mi 1,200 nm
228 mph 367 km/h cruise speed 520 kt 302 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.