de Havilland Canada DHC-2 Beaver vs. Lockheed Martin F-22 Raptor

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de Havilland Canada DHC-2 Beaver versus Lockheed Martin F-22 Raptor
13.56 m 44 ft 6 in length 18.9 m 62 ft 1 in
5 m 16 ft 5 in height 5.1 m 16 ft 9 in
16.56 m 54 ft 4 in wingspan 13.6 m 44 ft 7 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines Two Pratt & Whitney F119-PW-100 turbofan engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 35,000-pound class
Approximately 6,200 hp (4,624 kW) total total thrust 70,000-pound class
24,200 lb 10,977 kg MTOW 38,000 kg 83,500 lb
2,535 km 1,369 nm range 1,850 mi 1,611 nm
228 mph 367 km/h cruise speed Mach 1.6 1976 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.