McDonnell-Douglas MD-11 vs. Lockheed F-104 Starfighter

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McDonnell-Douglas MD-11 versus Lockheed F-104 Starfighter
61.20 m 200 ft 10 in length 16.69 m 54 ft 9 in
17.6 m 57 ft 9 in height 4.11 m 13 ft 6 in
51.6 m 169 ft 4 in wingspan 6.68 m 21 ft 11 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 1 Turbojet Engine
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 46.7 / 71.2 kN (dry/with Afterburner)
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 46.7 / 71.2 kN (dry/with Afterburner)
285,990 kg 630,400 lb MTOW 13,500 kg 29,800 lb
13,231 km 7,147 nm range 1,200 km 648 nm
961 km/h 597 mph cruise speed 510 mph 821 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.