Comparison of Airbus A321 and Kawasaki C-2 [S]ave
| Attribute |  Kawasaki C-2 × |  Airbus A321 × |
|---|---|---|
| General | ||
| Manufacturer | Kawasaki | Airbus |
| Model | Kawasaki C-2 | Airbus A321 |
| Country | Japan | France |
| Manufactured from (year) | 2010 | 1994 |
| Type | Military Transport Planes | Mid Size Passenger Jets |
| Icao | EC45 | - |
| Performance | ||
| Engine | 2x General Electric CF6-80C2K1F | 2 X CFM56-5 - |
| Power, lbf (lbf) | 59,740 | 56,200 |
| Avionics | - | Thales Avionics Suite |
| Max cruise speed (km/h) | 926 | 1,004 |
| Travel range (km) | 10,001 | 5,926 |
| Fuel economy (km/l) | - | 0.22 |
| Service ceiling (m) | 12,192 | 11,887 |
| Rate of climb (m/sec) | 17.78 | 0.06 |
| Take off distance (m) | 500 | 1,707 |
| Landing distance (m) | 500 | 1,540 |
| Weights | ||
| Max take off weight (kg) | 141,400 | 93,500 |
| Max payload (kg) | 37,600 | 21,725 |
| Fuel tank capacity (l) | 43,002 | 29,681 |
| Baggage volume (m³) | 251 | 51.76 |
| Dimensions | ||
| Seats | 3 | 22 |
| Seats - business class | - | 185 |
| Cabin height (m) | 4 | 2.22 |
| Cabin width (m) | 4 | 3.7 |
| Cabin length (m) | 16 | 34.44 |
| Exterior length (m) | 43.9 | 44.51 |
| Tail height (m) | 14.2 | - |
| Fuselage diameter (m) | 5 | 3.96 |
| Wing span (m) | 44.4 | 34.1 |
| Wing tips | No Winglets | No Winglets |
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