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Contents

   



(Top)
 


1 Design  





2 Development  





3 Operators  





4 Specifications (Ro.51 second prototype)  





5 See also  





6 References  





7 Further reading  





8 External links  














IMAM Ro.51






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From Wikipedia, the free encyclopedia
 


Ro.51
Role Fighter
Manufacturer IMAM
First flight 1937
Status Prototype
Number built 2

The IMAM Ro.51 was an Italian fighter aircraft that first flew in 1937. It was designed for the 1936 new fighter contest for the Regia Aeronautica, with practically all the Italian aircraft builders involved.

Design

[edit]

The aircraft, designed by the engineer Galasso, was a single-seat, monoplane fighter, of mixed construction (the wings were made of wood), and initially with a fixed undercarriage.

The engine was standard for this generation of fighters, an 840 hp (630 kW) Fiat A.74 RC 38 radial powering a three-blade propeller.

The fixed undercarriage limited the maximum speed to only 467 km/h. It was armed with two Breda-SAFAT 12.7 mm machine guns.

Development

[edit]

In June 1938 the first prototype, initially fitted with a very small tail, was tested and found inferior to the Macchi C.200 and Fiat G.50. It was overall a poor aircraft. The trials to re-engineer the wing came too late and no orders were made.

The second prototype Ro.51/1, featured a retractable landing gear which boosted its top speed to 489 km/h. It was later converted into a fighter floatplane. Like the Ro.44 it had a large central float and two smaller ones under the wings. The maximum speed dropped to 430 km/h, but endurance was increased to 1,200 km.

Unfortunately during a trial one of the wings suddenly sank in the water. The rest of the aircraft swiftly followed, and the loss of this prototype meant the end of the program. Although performance was apparently fairly good, the project was overall a failure, especially in the early aspects, even if it was not too different from the Fokker D.XXI. But with so many other superior machines also involved, waiting for the problems the Ro.51 had to be fixed was not an option.

Operators

[edit]
 Kingdom of Italy

Specifications (Ro.51 second prototype)

[edit]

Data from The Complete Book of Fighters,[1] Italian Civil and Military Aircraft 1930-1945,[2] airwar.ru : IMAM Ro.51[3]

General characteristics

Performance

Armament

See also

[edit]

Aircraft of comparable role, configuration, and era

Related lists

References

[edit]
  1. ^ Green, W; Swanborough, G (1994). The Complete Book of Fighters. New York: Smithmark. pp. 308–309. ISBN 0-8317-3939-8.
  • ^ Thompson, Jonathon W. (1963). Italian Civil and Military Aircraft 1930-1945. USA: Aero Publishers Inc. pp. 206–209. ISBN 0-8168-6500-0.
  • ^ "IMAM Ro.51" (in Russian). Retrieved 26 December 2019.
  • Further reading

    [edit]
    [edit]
  • Companies
  • Aviation

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=IMAM_Ro.51&oldid=1222547227"

    Categories: 
    IMAM aircraft
    1930s Italian fighter aircraft
    Abandoned military aircraft projects of Italy
    Single-engined tractor aircraft
    Low-wing aircraft
    Floatplanes
    Aircraft first flown in 1937
    Hidden categories: 
    CS1 Russian-language sources (ru)
    Articles with short description
    Short description is different from Wikidata
    Articles with Italian-language sources (it)
    Commons category link is on Wikidata
    Webarchive template wayback links
     



    This page was last edited on 6 May 2024, at 15:44 (UTC).

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