Airbus A321LR vs. de Havilland Venom
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| Airbus A321LR |
versus |
de Havilland Venom |
| 44.51 m |
146 ft 0 in |
length |
6.71 m |
22 ft 0 in |
| 11.76 m |
38 ft 7 in |
height |
1.88 m |
6 ft 2 in |
| 35.8 m |
117 ft 5 in |
wingspan |
12.7 m |
41 ft 8 in |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 (de Havilland Ghost 105) |
| Over 33,000 lbs (147 kN) |
thrust per engine |
23.6 kN |
| 66,000 lbs (294 kN) |
total thrust |
23.6 kN |
| 97,000 kg |
213,800 lb |
MTOW |
6,945 kg |
15,300 lb |
| 7,400 km |
4,000 nm |
range |
1,730 km |
935 nm |
| 832 km/h |
517 mph |
cruise speed |
1030 km/h |
640 mph |
| 180-220 passengers |
capacity |
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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.
