Airbus A321LR vs. North American F-100 Super Sabre
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here.
| Airbus A321LR |
versus |
North American F-100 Super Sabre |
| 44.51 m |
146 ft 0 in |
length |
16.46 m |
54 ft 2 in |
| 11.76 m |
38 ft 7 in |
height |
4.93 m |
16 ft 2 in |
| 35.8 m |
117 ft 5 in |
wingspan |
11.84 m |
38 ft 1 |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 Pratt & Whitney J57-P-21A |
| Over 33,000 lbs (147 kN) |
thrust per engine |
16,000 lb. thrust in afterburner |
| 66,000 lbs (294 kN) |
total thrust |
16,000 lb. (afterburner) |
| 97,000 kg |
213,800 lb |
MTOW |
17,609 kg |
38,800 lb |
| 7,400 km |
4,000 nm |
range |
2,673 km |
1,444 nm |
| 832 km/h |
517 mph |
cruise speed |
587 mph |
945 km/h |
| 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.
