Attribute | Value |
---|---|
General | |
Manufacturer | Curtiss |
Model | Curtiss P-36 Hawk |
Country | United States |
Manufactured from | 1938 year |
Manufactured to | 1944 year |
Type | Military Propellor Planes |
Icao | P36 |
Performance | |
Engine | 1x Pratt & Whitney R-1830-17 Twin Wasp |
Power, hp | 1,050 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 504 km/h |
Approach speed | 120 km/h |
Travel range | 1,389 km |
Fuel economy | Add |
Service ceiling | 10,058 m |
Rate of climb | 17.27 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 2,726 kg |
Max landing weight | 2,563 kg |
Max payload | 550 kg |
Fuel tank capacity | 511 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 | 8.7 m |
Tail height | 2.84 m |
Fuselage diameter | 1.2 m |
Wing span | 11.38 m |
Wing tips | No Winglets |