Airbus A321LR vs. Lockheed C-69 Constellation
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| Airbus A321LR |
versus |
Lockheed C-69 Constellation |
| 44.51 m |
146 ft 0 in |
length |
29.72 m |
97 ft 6 in |
| 11.76 m |
38 ft 7 in |
height |
6.02 m |
19 ft 9 in |
| 35.8 m |
117 ft 5 in |
wingspan |
37.49 m |
123 ft |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
4 x Wright R-3350 Duplex-Cyclone radial engines |
| Over 33,000 lbs (147 kN) |
thrust per engine |
2,200 to 3,700 horsepower (1,640 to 2,760 kW) |
| 66,000 lbs (294 kN) |
total thrust |
8,800 to 14,800 horsepower |
| 97,000 kg |
213,800 lb |
MTOW |
44,453 kg |
98,000 lb |
| 7,400 km |
4,000 nm |
range |
5,200 km |
2,808 nm |
| 832 km/h |
517 mph |
cruise speed |
507 km/h |
315 mph |
| 180-220 passengers |
capacity |
Up to 109 passengers |
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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.
