de Havilland Canada DHC-2 Beaver vs. Lockheed F-104 Starfighter

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de Havilland Canada DHC-2 Beaver versus Lockheed F-104 Starfighter
13.56 m 44 ft 6 in length 16.69 m 54 ft 9 in
5 m 16 ft 5 in height 4.11 m 13 ft 6 in
16.56 m 54 ft 4 in wingspan 6.68 m 21 ft 11 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 Turbojet Engine
Approximately 3,100 hp (2,312 kW) each thrust per engine 46.7 / 71.2 kN (dry/with Afterburner)
Approximately 6,200 hp (4,624 kW) total total thrust 46.7 / 71.2 kN (dry/with Afterburner)
24,200 lb 10,977 kg MTOW 13,500 kg 29,800 lb
2,535 km 1,369 nm range 1,200 km 648 nm
228 mph 367 km/h cruise speed 510 mph 821 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.