Piaggio P.119
| GENERAL DATA | |||
| Other Designation(s) | - |
||
| Type |
Fighter |
Crew | 1 |
| Manufacturer(s) | Piaggio |
||
| Production | 1 |
||
| Prototype first flight | 19 December 1942 |
Status | Prototype only |
| DIMENSIONS | |||
| Length | 9.70 m |
Empty Weight | 2438 kg |
| Wingspan | 13 m |
Loaded Weight | ? kg |
| Height | 2.90 m |
Max takeoff weight | 4091 kg |
| Wing area | 27.8 m² |
Wing loading | 147 kg/m² |
| ARMAMENT | ||||
| Main Gun | Hub mounted |
1 × 20 mm (0.787 in) Breda-SAFAT
cannon |
Ammunition Carried |
1 x 110 |
| Secondary Guns | Nose mounted |
4 × 12.7 mm (0.500 in) Breda-SAFAT MG |
Ammunition Carried | 4 x 500-550 |
| Bombs | - |
|||
| POWERPLANT | |||
| Engine | 1 ×
Piaggio P.XV RC.45 |
Type & Displacement | 18-cyl. air-cooled radial piston,
53.0 L |
| Horsepower (maximum) | 1500 hp |
Power/Weight Ratio | 366.65 hp / ton * |
| Fuel Capacity | 1000 L
|
||
(*) Max takeoff weight
| PERFORMANCES | |||
| Maximum Speed | 644 km/h
at 6795 m |
Cruise Speed | ? km/h |
| Landing Speed | 130 km/h |
Service Ceiling | 12603 m |
| Rate of Climb | 15.6 m/s |
Range | 1513 km |
| Sources | |||
| Wikipédia | militaryfactory.com | ||
Drawings |
