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Bloch MB.210

From Wikipedia, the free encyclopedia
1934 bomber aircraft family by Avions Marcel Bloch
MB.210 / MB.211
An MB.210
General information
TypeBomber
ManufacturerSociété des Avions Marcel Bloch
Built byVarious, including:
Les Mureaux
Potez-CAMS
Breguet
Hanriot
Renault
Statusretired
Primary userFrench Air Force
Number built< 300
History
Introduction dateNovember 1936
First flight23 November 1934
Retiredaround 1945
Developed fromBloch MB.200

TheBloch MB.210 andMB.211 were the successors of the FrenchBloch MB.200bomber developed bySociété des Avions Marcel Bloch in the 1930s and differed primarily in being low wing monoplanes rather than high wing monoplanes.

Development

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The MB.210 derived from theMB.200 and differs in particular by having itscantilever wing set at the bottom of the fuselage, and in having a retractableundercarriage. Developed as a private venture, theprototype MB.210 accomplished its first flight on 23 November 1934, powered by two 596 kW (800 hp)Gnome-Rhône 14Kdrs /Gnome-Rhône 14Kgrs air-cooledradial engines and having a fixed undercarriage. This was followed by a second prototype, theMB.211 Verdun, powered by 641 kW (860 hp)Hispano-Suiza 12Y V-12 liquid-cooledinlines and fitted with a retractable undercarriage, this flying on 29 August 1935. Initial flight testing of this version was somewhat disappointing, so no further examples were built. Further progress with the MB.210, however, convinced theArmée de l'Air to order series production, the first example of which flew on 12 December 1936.[1]

The satisfaction did not last very long, however, since it was underpowered and the engines of production aircraft were inclined to overheating. The type was grounded until its engines could be replaced by the more powerful and reliableGnome-Rhône 14N, these engines first being tested in summer 1937 and had to be replaced.[2] Altogether, 257 units were manufactured amongst companies as diverse asLes Mureaux overPotez-CAMS,Breguet,Hanriot, andRenault.

Operational history

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Bloch MB.210 of theSpanish Republican Air Force

In September 1939, the Bloch MB.210 equipped 12 bomber units of theArmée de l'Air. At the time ofNazi Germany'sattack on France in spring 1940, these squadrons were in the middle of a restructuring aimed at removing outdated aircraft from the front line. Up to the armistice on 25 June of the same year, the MB.210 was used still for nighttime bombing missions and shifted then toNorth Africa.

Variants

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MB.211 prototype at the 1934Paris Air Show
MB.210.01
First prototype, powered by 2× 596 kW (800 hp)Gnome-Rhône 14Kdrs /Gnome-Rhône 14Kgrs air-cooledradial engines
MB.210Bn.4
Initial production version, powered by 2×Gnome-Rhône 14N-10 /Gnome-Rhône 14N-11 radial engines
MB.210Bn.5
Hanriot-built variant with extra crew member
MB.210H
Floatplane version powered by 2×Gnome-Rhône 14Kirs engines
MB.211.01
Prototype equipped with two 641 kW (860 hp)Hispano-Suiza 12Y inline engines
MB.212
project[3]
MB.218
project[3]

Operators

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 Bulgaria
Bulgarian Air Force – Received six aircraft from Germany.[3]
 France
Germany
Luftwaffe – Used briefly for training in 1942 after theGerman occupation of France
 Romania
Royal Romanian Air Force – Received 10 from an order of 24.[3]
SpainSpain
Spanish Republican Air Force received at least three[4] aircraft.[5]

Specifications (MB.210Bn.5)

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Data fromWar Planes of the Second World War: Volume Seven[6]

General characteristics

  • Crew: 5
  • Length: 18.83 m (61 ft 9 in)
  • Wingspan: 22.82 m (74 ft 10 in)
  • Height: 6.7 m (22 ft 0 in)
  • Wing area: 62.5 m2 (673 sq ft)
  • Empty weight: 6,413 kg (14,138 lb)
  • Gross weight: 9,720 kg (21,429 lb)
  • Max takeoff weight: 10,221 kg (22,533 lb)
  • Powerplant: 1 ×Gnome-Rhône 14N-10 14-cylinder air-cooledradial engine, 709 kW (950 hp) LH rotation
  • Powerplant: 1 ×Gnome-Rhône 14N-11 14-cylinder air-cooledradial engine, 709 kW (950 hp) RH rotation
  • Propellers: 3-bladed variable-pitch propellers (LH and RH rotation)

Performance

  • Maximum speed: 322 km/h (200 mph, 174 kn) at 3,500 m (11,500 ft)
  • Cruise speed: 240 km/h (150 mph, 130 kn) econ. at 3,500 m (11,500 ft)
  • Range: 1,700 km (1,100 mi, 920 nmi)
  • Service ceiling: 9,900 m (32,500 ft)
  • Time to altitude: 4,000 m (13,000 ft) in 12 minutes
  • Wing loading: 156 kg/m2 (32 lb/sq ft)
  • Power/mass: 0.15 kW/kg (0.091 hp/lb)

Armament

  • Guns: 3 × 7.5 mm (.295 in)MAC 1934 machine guns (one in nose, dorsal and ventral turrets)
  • Bombs: 1,600 kg (3,520 lb) of bombs

See also

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Related development

Related lists

Notes

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  1. ^Green 1967, pp. 124–126.
  2. ^Green 1967, p. 127.
  3. ^abcd"Bloch MB 210–211."dassault-aviation.com. Retrieved: 2 November 2011.
  4. ^BLOCH 200/210Archived March 19, 2012, at theWayback Machine
  5. ^MB 210-211Archived 2012-05-23 at theWayback Machine. Dassault Aviation. Retrieved 17 August 2008.
  6. ^Green 1967, p. 128.

Bibliography

[edit]
  • Green, William (1967).War Planes of the Second World War: Bombers and Reconnaissance Aircraft; Australia, Belgium, Bohemia-Moravia, Bulgaria, Canada, Finland, France. Vol. VII. London: Macdonald.OCLC 369132578.

Further reading

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  • Comas, Matthieu (September 2000). "Les bombardiers polonais de Lyon-Bron" [The Polish Bombers of Lyon-Bron].Avions: Toute l'Aéronautique et son histoire (in French) (90):30–32.ISSN 1243-8650.
  • Fernandez, José (August 1994). "Le Bloch MB 210 (5ème partie)" [The Bloch MB 210, Part 5].Avions: Toute l'aéronautique et son histoire (in French) (18):2–5.ISSN 1243-8650.
  • Fernandez, José (September 1994). "Le Bloch MB 210 (6ème partie)" [The Bloch MB 210, Part 6].Avions: Toute l'aéronautique et son histoire (in French) (19):37–39.ISSN 1243-8650.

External links

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Wikimedia Commons has media related toBloch MB.210.
Bloch aircraft
Designation Sequence
Transports
Bombers
Fighters
Floatplanes
Light civil aircraft
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