Attribute | Value |
---|---|
General | |
Manufacturer | Glenn L. Martin Company |
Model | Martin B-10 |
Country | United States |
Manufactured from | 1933 year |
Manufactured to | 1940 year |
Type | Military Propellor Planes |
Icao | B10 |
Performance | |
Engine | 2x Wright R-1820-33 Cyclone |
Power, hp | 775 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 343 km/h |
Approach speed | Add |
Travel range | 2,000 km |
Fuel economy | Add |
Service ceiling | 7,376 m |
Rate of climb | 7.01 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 7,440 kg |
Max landing weight | Add |
Max payload | 1,025 kg |
Fuel tank capacity | 2,801 l |
Baggage volume | Add |
Dimensions | |
Seats | 3 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 13.64 m |
Tail height | 4.7 m |
Fuselage diameter | 1.3 m |
Wing span | 21.5 m |
Wing tips | No Winglets |