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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]
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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