Comparison of Focke-Wulf Ta 152 and Mitsubishi A6M Zero [S]ave
| Attribute |  Focke-Wulf Ta 152 × |  Mitsubishi A6M Zero × |
|---|---|---|
| General | ||
| Manufacturer | Focke-Wulf | Mitsubishi Heavy Industries |
| Model | Focke-Wulf Ta 152 | Mitsubishi A6M Zero |
| Country | Germany | Japan |
| Manufactured from (year) | 1944 | 1939 |
| Manufactured to (year) | 1945 | 1945 |
| Type | Military Propellor Planes | Military Propellor Planes |
| Icao | TA152 | A6M |
| Performance | ||
| Engine | 1x Junkers Jumo 213E | 1x Mitsubishi NK1F Sakae 21 |
| Power, hp (hp) | 1,750 | 1,130 |
| Max cruise speed (km/h) | 759 | 533 |
| Approach speed (km/h) | 180 | 111 |
| Travel range (km) | 2,037 | 1,871 |
| Service ceiling (m) | 15,088 | 10,058 |
| Rate of climb (m/sec) | 19.81 | 15.7 |
| Weights | ||
| Max take off weight (kg) | 5,217 | 2,796 |
| Max payload (kg) | - | 270 |
| Fuel tank capacity (l) | 992 | 848 |
| Dimensions | ||
| Seats | 1 | 1 |
| Exterior length (m) | 10.82 | 9.06 |
| Tail height (m) | 4 | 3.05 |
| Fuselage diameter (m) | 1.1 | 1.1 |
| Wing span (m) | 14.5 | 12 |
| Wing tips | No Winglets | No Winglets |
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