Airbus A321LR vs. McDonnell Douglas F-4 Phantom II
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| Airbus A321LR |
versus |
McDonnell Douglas F-4 Phantom II |
| 44.51 m |
146 ft 0 in |
length |
19.2 m |
63 ft 0 in |
| 11.76 m |
38 ft 7 in |
height |
5.03 m |
16 ft 6 in |
| 35.8 m |
117 ft 5 in |
wingspan |
11.72 m |
38 ft 5 in |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
Two General Electric J79s |
| Over 33,000 lbs (147 kN) |
thrust per engine |
17,900 lbs |
| 66,000 lbs (294 kN) |
total thrust |
35,800 lbs |
| 97,000 kg |
213,800 lb |
MTOW |
27,965 kg |
61,700 lb |
| 7,400 km |
4,000 nm |
range |
3,031 km |
1,636 nm |
| 832 km/h |
517 mph |
cruise speed |
Mach 2.2 |
2,717 km/h |
| 180-220 passengers |
capacity |
Up to 16,000 lbs of externally carried ordnance |
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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.
