Bloch MB.152
| GENERAL DATA | |||
| Other Designation(s) | - |
||
| Type | Fighter |
Crew | 1 |
| Manufacturer(s) | SNCASO |
||
| Production | Total: 657 - Bloch
MB 150: 1, Bloch MB 151: 140, Bloch
MB 152: 482, 614, Bloch MB 153: 1, Bloch
MB 155: 33 |
||
| First Flight | 15 December 1938 |
Introduction | 1939 |
| Variants | |||
| MB. 152 | Production model. | ||
| MB. 153 | Had Pratt & Whitney R-1830 Twin Wasp engine (1050 hp). | ||
| MB. 155 | MB.155.01 prototype converted from a MB.152 and MB.155.C1
production versions powered by Gnome-Rhône 14N-49 engines (33 built) |
||
| MB. 157 | Single prototype of advanced version, converted from the MB.152 and equipped with a 1580hp Gnome-Rhône 14R-4 engine. | ||
| DIMENSIONS | |||
| Empty Weight | 2158 kg |
Loaded Weight | 2693 kg |
| Max takeoff weight | 2800 kg |
Length | 9.1 m |
| Wingspan | 10.54 m |
Wing area | 17.32 m² |
| Height | 3.03 m |
Wing Loading | 155.4 kg/m² |
| ARMAMENT | |||
| Main Guns | 2 × 20 mm Hispano-Suiza HS.404* |
Ammunition Carried | 2 x 60 |
| Secondary Guns | 2 × 7.5 mm (0.295 in) M39 MAC 1934** |
Ammunition Carried | 2 x 500 |
| Other Armament | - |
||
(*) or 2 × 7.5 mm (0.295 in) M39 MAC 1934 (2 x 500 rounds), (*,**) mounted in wings
| POWERPLANT | |||
| Engine | 1 × 1 × Gnome-Rhône
14N-25 * |
Type & Displacement | 4-cyl. two-row air-cooled radial,
38.67 L |
| Horsepower (maximum) | 1080
hp |
Power/Weight Ratio | 401.04 hp / ton ** |
| Fuel Capacity | Fuel
capacity internal: 427 liters, Fuel capacity external:
? liters
|
||
(*) or 1 x Gnome-Rhône 14N-49 engine rated at 1100 hp, (**) with loaded weight
| PERFORMANCES | |||
| Maximum Speed | 509 km/h |
Cruising Speed | 450 km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 10000 m |
| Rate of Climb | 9.36 m/s |
Range | 540 km, 600 km, 935 km |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | - | - |
|
Drawings |
