McDonnell-Douglas MD-11 vs. Lockheed Martin F-22 Raptor

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McDonnell-Douglas MD-11 versus Lockheed Martin F-22 Raptor
61.20 m 200 ft 10 in length 18.9 m 62 ft 1 in
17.6 m 57 ft 9 in height 5.1 m 16 ft 9 in
51.6 m 169 ft 4 in wingspan 13.6 m 44 ft 7 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines Two Pratt & Whitney F119-PW-100 turbofan engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 35,000-pound class
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 70,000-pound class
285,990 kg 630,400 lb MTOW 38,000 kg 83,500 lb
13,231 km 7,147 nm range 1,850 mi 1,611 nm
961 km/h 597 mph cruise speed Mach 1.6 1976 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.