SE.100
| GENERAL DATA | |||
| Other Designation(s) | LeO.50 |
||
| Type | Heavy Fighter |
Crew | 2-3 |
| Manufacturer(s) | Lioré
et Olivier, SNCASE |
||
| Production | 1 |
||
| First Flight | 29 March 1939 |
Introduction | Late 1940 (planned) |
| DIMENSIONS | |||
| Length | 11.8 m |
Empty Weight | 5520 kg |
| Wingspan | 15.7 m |
Loaded Weight | 7500 kg |
| Height | 4.28 m |
Max takeoff weight | ? kg |
| Wing area | 33 m² |
Wing Loading | 227 kg/m² |
| ARMAMENT (Prototype) | |||
| Main Guns | 4 x 20 mm Hispano-Suiza HS.404 * |
Ammunition Carried | 4 x ? |
1 x 20 mm Hispano-Suiza HS.404 ** |
1 x ? |
||
| Secondary Guns | - |
Ammunition Carried | - |
| Other Armament | - |
||
(*) in nose, (**) in rear gunner's post
| ARMAMENT (Planned Production version) | |||
| Main Guns | 6 x 20 mm Hispano-Suiza HS.404 * |
Ammunition Carried | 6 x ? |
2 x 20 mm Hispano-Suiza HS.404 ** |
2 x ? |
||
2 x 20 mm Hispano-Suiza HS.404 *** |
2 x ? |
||
| Secondary Guns | - |
Ammunition Carried | - |
| Other Armament | - |
||
(*) in nose, (**) in a rear turret, (***) in the belly
| POWERPLANT | |||
| Engine | 1 × Gnome-Rhône 14N-20 (LH rotation) |
Type & Displacement | 14-cyl. air-cooled radial piston, 38.67 L |
1 × Gnome-Rhône 14N-21
(RH rotation) |
14-cyl. air-cooled radial piston,
38.67 L |
||
| Horsepower (maximum) | 2
x 1081 hp |
Power/Weight Ratio | 265.96 hp / ton * |
| Fuel Capacity | ? L
|
||
(*) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 580 km/h at 6500 m |
Cruising Speed | 499 km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 8900-10000 m |
| Rate of Climb | ? m/s |
Range | 1300 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | avionslegendaires.net | ||
Drawings |
