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  • Bloch MB.210 Bomber Aircraft


    The Bloch 210 series represented the first true modern bomber design of the French Air Force leading up to World War 2.

     Updated: 6/7/2017; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com


    Societe des Avions Marcel Bloch, a French aviation concern, designed, developed and produced several pre-World War 2 aircraft in both civilian and military guises. Final civilian forms came in 1939, just prior to the Fall of France in the summer of 1940, while military versions persisted into 1947. By the end of World War 2, the concern had officially changed its name to Dassault Aviation, a name which continues in the aviation realm even today (2013). The original Bloch concern was founded by French aircraft engineer Marcel Bloch (1892-1986) who later had his last name legally changed to Dassault in response to the mass persecution of Jews in France under the Nazi-aligned Vichy French government.

    Bloch developed a high-winged, twin-engine bomber in the early 1930s which was adopted by several air powers of the day (inluding that of the French). This aircraft was designated as the MB.200 ("Marcel Bloch Model 200") and approximately 332 of the type were constructed from 1933 to 1939. The MB.200 was developed in response to a 1932 French Air Force requirement for a modern day/night-capable bomber. The series was eventually evolved into three other forms, each fitting various engine types.


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    Bloch MB.210Bn.5 Technical Specifications


    Service Year: 1935
    Type: Bomber Aircraft
    National Origin: France
    Manufacturer(s): Les Mureaux / Potez-CAMS / Breguet / Hanriot / Renault / Bloch - France
    Production Total: 300



    Structural (Crew Space, Dimensions and Weights)


    Operating Crew: 5
    Length: 61.78 feet (18.83 meters)
    Width: 74.87 feet (22.82 meters)
    Height: 21.98 feet (6.70 meters)

    Weight (Empty): 14,110 lb (6,400 kg)
    Weight (MTOW): 22,487 lb (10,200 kg)

    Installed Power and Standard Day Performance


    Engine(s): 2 x Gnome-Rhone 14N-10/-11 14-cylinder air-cooled radial piston engine developing 950 horsepower each.

    Maximum Speed: 200 mph (322 kph; 174 knots)
    Maximum Range: 1,056 miles (1,700 km)
    Service Ceiling: 32,480 feet (9,900 meters; 6.15 miles)
    Rate-of-Climb: 1,000 feet-per-minute (305 m/min)

    Armament / Mission Payload


    STANDARD:
    1 x 7.5mm MAC 1934 machine in nose position
    1 x 7.5mm MAC 1934 machine gun in dorsal position.
    1 x 7.5mm MAC 1934 machine gun in ventral position.

    OPTIONAL:
    Up to 3,500lbs of conventional drop bombs

    Global Operators / Customers


    Bulgaria; France; Nazi Germany; Romania; Spain

    Model Variants (Including Prototypes)


    MB.210.01

    MB.210Bn.4

    MB.210Bn.5

    MB.210H

    MB.211.01

    MB.212

    MB.218