Airbus A321-200 vs. Lockheed L-1011 TriStar 500
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Airbus A321-200 |
versus |
Lockheed L-1011 TriStar 500 |
44.51 m |
146 ft 0 in |
length |
50.05 m |
164 ft 3 in |
11.76 m |
38 ft 7 in |
height |
16.87 m |
55 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
50.09 m |
164 ft 4 in |
2 GE CFM56-5B3 |
engines |
3 Rolls-Royce RB211 engines |
31,600 lbs |
thrust per engine |
42,000 lbf |
63,200 lbs |
total thrust |
126,000 lbf (3 engines x 42,000 lbf per engine) |
89,000 kg |
196,200 lb |
MTOW |
231,330 kg |
510,000 lb |
4,000 nmi |
7,408 km |
range |
11,260 km |
6,100 nm |
871 km/h |
541 mph |
cruise speed |
525 knots |
972 km/h |
185 to 220 |
capacity |
Max. 315 passengers (typical 253) |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.