McDonnell-Douglas MD-11 vs. Lockheed SR-71 Blackbird

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McDonnell-Douglas MD-11 versus Lockheed SR-71 Blackbird
61.20 m 200 ft 10 in length 32.74 m 107 ft 5 in
17.6 m 57 ft 9 in height 5.64 m 18 ft 6 in
51.6 m 169 ft 4 in wingspan 16.94 m 55 ft 7 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines Two Pratt & Whitney J58 axial-flow turbojets
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 34,000 lbs
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 68,000 lbs
285,990 kg 630,400 lb MTOW 78,018 kg 172,000 lb
13,231 km 7,147 nm range 3,250 mi 2,832 nm
961 km/h 597 mph cruise speed Mach 3.2 3951 km/h
Max 410 passengers 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.