McDonnell-Douglas MD-11 vs. Lockheed T-33 Shooting Star

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McDonnell-Douglas MD-11 versus Lockheed T-33 Shooting Star
61.20 m 200 ft 10 in length 11.51 m 37 ft 9 in
17.6 m 57 ft 9 in height 3.56 m 11 ft 8 in
51.6 m 169 ft 4 in wingspan 11.9 m 39 ft 1 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 1 (Allison J33-A-5)
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 24.0 kN
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 24.0 kN
285,990 kg 630,400 lb MTOW 5,900 kg 13,000 lb
13,231 km 7,147 nm range 2,050 km 1,107 nm
961 km/h 597 mph cruise speed 965 km/h 600 mph
Max 410 passengers capacity 907 kg of bombs or rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.