McDonnell-Douglas MD-11 vs. Concorde
... or view the full comparison list
here.
McDonnell-Douglas MD-11 |
versus |
Concorde |
61.20 m |
200 ft 10 in |
length |
61.66 m |
202 ft 4 in |
17.6 m |
57 ft 9 in |
height |
11.4 m |
37 ft 5 in |
51.6 m |
169 ft 4 in |
wingspan |
25.56 m |
83 ft 1 |
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
engines |
4 Rolls Royce/Snecma Olympus 593 turbo jet engines |
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
thrust per engine |
18.7 tons (180 kN) |
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
total thrust |
74.8 tons (720 kN) |
285,990 kg |
630,400 lb |
MTOW |
185,000 kg |
408,000 lb |
13,231 km |
7,147 nm |
range |
6,580 km |
3,554 nm |
961 km/h |
597 mph |
cruise speed |
Mach 2.04 |
2,179 km/h |
Max 410 passengers |
capacity |
92–120 passengers |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.