de Havilland Canada DHC-2 Beaver vs. Lockheed SR-71 Blackbird

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de Havilland Canada DHC-2 Beaver versus Lockheed SR-71 Blackbird
13.56 m 44 ft 6 in length 32.74 m 107 ft 5 in
5 m 16 ft 5 in height 5.64 m 18 ft 6 in
16.56 m 54 ft 4 in wingspan 16.94 m 55 ft 7 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines Two Pratt & Whitney J58 axial-flow turbojets
Approximately 3,100 hp (2,312 kW) each thrust per engine 34,000 lbs
Approximately 6,200 hp (4,624 kW) total total thrust 68,000 lbs
24,200 lb 10,977 kg MTOW 78,018 kg 172,000 lb
2,535 km 1,369 nm range 3,250 mi 2,832 nm
228 mph 367 km/h cruise speed Mach 3.2 3951 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.