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BREGUET Br482

 


Technical Specifications
Type
Four-seater four-engine heavy bomber with low wings and retractable gear
Date first flight
November 1947
Wingspan
24.20m
Lenght
18.75m
Height
4.40m
Wing Area
67.40m
Empty Weight
9456kg
Max. Takeoff Weight
16000 kg
Cruising Speed
Maximum Speed
525 km/h at 5000m
Climbing Speed
Service ceilling
12000m
Range
1600 kms
Crew
4 Men
Motorization
4 Engine Hispano-Suiza 12 Y-51 à 12 Cylinder inline liquid-cooled of1100 Hp on take-off
Armament
1 Machine-gun MAC of 7.5mm on carriage in the nose
1 Cannon Hispano-Suiza of 20mm in a dorsal position
2 Machine-guns MAC of 7.5mm on separed carriage in ventral position
2500kg of bombs bay

 


Production

Two prototypes, Nos. 01 and 02, were built at the beginning of 1940.

 


Historical

The Breguet 482 was born from the program A21 of December 1936. This first concerned a project of B4 twin-engined engines equipped with engines Gnome Rhone (1934), program then extended to four-engines. The Breguet 482 was in competition with the Bloch 135, another four-engine. The Breguet Br 482 was equipped with Hispano-Suiza 12Y-20/21 engines.

Although commissioned in May 1938, construction of the two prototypes did not begin until 1939, with new Hispano-Suiza HS 12 Y-50/51 engines of 1100 CV. The aircraft was of modern design, all steel with a monocoque fuselage.

Surprised by the German advance, the two prototypes were evacuated: one to North Africa, where it was destroyed during the Allied landing in 1942, the other to Toulouse where it was stored throughout the occupation.

It was not until 1947 that the latter was completed, and that he made his first flight. It was then used as a test aircraft.


Bibliography

1) _ Editions Larivière :
- Le Fanatique de L'Aviation : No339

 


Photos Album

 


Drawing 3 views