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Viberti Musca 1

Type of aircraft From Wikipedia, the free encyclopedia

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The Viberti Musca 1 is a 1940s Italian two-seat civil touring monoplane produced by Ali Verberti SpA of Turin.[1]

Quick Facts Role, National origin ...

The Musca 1 was a cantilever low-wing monoplane powered by an 85 hp (63 kW) Continental C85 flat-four piston engine.[1] Named for the chief designer Franco Muscariello it had an enclosed side-by-side seating and a fixed conventional landing gear.[1] The Musca 1 started production in 1948 and in 1951 the Musca 1bis was introduced with structural improvements.[1] The company had two further variants planned but the company was dissolved around 1951.[1] Muscareillo continued development of the Musca 1, however, flying a modified version, the Musca 1 Ter powered by a Walter Micron on 15 September 1952.[2][3]

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Variants

Musca 1
Initial production variant.
Musca 1bis
Structural improvements.
Musca 1 Ter
Modified undercarriage and 75 horsepower (56 kW) Walter Micron III engine.[2]
Musca 2
Three-seat cabin monoplane, not built.
Musca 4
A high-wing development of the Musca 1, not built.

Specifications

Data from Jane's All The World's Aircraft 1951–52.[4]

General characteristics

  • Crew: 2
  • Length: 6.65 m (21 ft 10 in)
  • Wingspan: 9.50 m (31 ft 2 in)
  • Empty weight: 580 kg (1,279 lb)
  • Powerplant: 1 × Continental C85 four-cylinder air-cooled horizontally-opposed engine, 63 kW (85 hp)

Performance

  • Maximum speed: 178 km/h (111 mph, 96 kn) at 1,800 m (5,900 ft)
  • Cruise speed: 130 km/h (81 mph, 70 kn)
  • Stall speed: 60 km/h (37 mph, 32 kn)

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References

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