Martin 2-0-2 [+]Compare [E]dit [H]istory
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| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Glenn L. Martin Company |
| Model | Martin 2-0-2 |
| Country | United States |
| Manufactured from | 1946 year |
| Manufactured to | 1948 year |
| Type | Passenger Turbo Props |
| Icao | Add |
| Performance | |
| Engine | 2x Pratt & Whitney R-2800 CA-18 Double Wasp |
| Power, hp | 2,400 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 500 km/h |
| Approach speed | 122 km/h |
| Travel range | 1,022 km |
| Fuel economy | Add |
| Service ceiling | 10,058 m |
| Rate of climb | 11.18 m/sec |
| Take off distance | 477 m |
| Landing distance | 520 m |
| Weights | |
| Max take off weight | 18,098 kg |
| Max landing weight | Add |
| Max payload | 4,200 kg |
| Fuel tank capacity | 6,587 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 4 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 21.74 m |
| Tail height | 8.66 m |
| Fuselage diameter | 2.8 m |
| Wing span | 28.42 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 (39 fields were changed)
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