North American P-51 Mustang [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | North American Aviation NAA |
| Model | North American P-51 Mustang |
| Country | United States |
| Manufactured from | 1940 year |
| Manufactured to | 1945 year |
| Type | Military Propellor Planes |
| Icao | P51 |
| Performance | |
| Engine | 1x Packard (Rolls Royce) V-1650-7 Merlin |
| Power, hp | 1,720 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 709 km/h |
| Approach speed | 161 km/h |
| Travel range | 2,656 km |
| Fuel economy | Add |
| Service ceiling | 12,771 m |
| Rate of climb | 16.26 m/sec |
| Take off distance | 366 m |
| Landing distance | 457 m |
| Weights | |
| Max take off weight | 5,490 kg |
| Max landing weight | 5,490 kg |
| Max payload | 910 kg |
| Fuel tank capacity | 1,018 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 1 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 9.8 m |
| Tail height | 4.08 m |
| Fuselage diameter | 0.9 m |
| Wing span | 11.28 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (41 fields were changed)
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