Airbus A321LR vs. Mitsubishi A6M Zero
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here.
| Airbus A321LR |
versus |
Mitsubishi A6M Zero |
| 44.51 m |
146 ft 0 in |
length |
9.06 m |
29 ft 9 in |
| 11.76 m |
38 ft 7 in |
height |
3.05 m |
10 ft |
| 35.8 m |
117 ft 5 in |
wingspan |
12 m |
39 ft 4 in |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine |
| Over 33,000 lbs (147 kN) |
thrust per engine |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
| 66,000 lbs (294 kN) |
total thrust |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
| 97,000 kg |
213,800 lb |
MTOW |
2,800 kg |
6,170 lb |
| 7,400 km |
4,000 nm |
range |
1,010 nm |
1,871 km |
| 832 km/h |
517 mph |
cruise speed |
180 knots |
105 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.
