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Boisavia Muscadet

Type of aircraft From Wikipedia, the free encyclopedia

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The Boisavia B.50 Muscadet was a prototype French three-seat cabin monoplane first flown in 1946.[1]

Quick facts B.50 Muscadet, Role ...

Design and operations

The B.50 was designed and built after the Second World War by Luicien Tieles, it was a strut-braced high-wing monoplane with three seats and a conventional landing gear with a tail wheel.[1] The prototype, with the French test registration F-WCZE, first flew on 13 October 1946 powered by a 100 hp (75 kW) Renault 4Pei engine.[1] Tieles modified the design as a four-seater and formed Societe Boisavia to build the type which he called the Mercurey.[1]

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Specifications

Data from Gaillard (1990) p. 40[2]

General characteristics

  • Crew: One pilot
  • Capacity: One passenger
  • Length: 7.15 m (23 ft 5 in)
  • Wingspan: 10.50 m (34 ft 5 in)
  • Height: 2.20 m (7 ft 3 in)
  • Wing area: 15 m2 (160 sq ft)
  • Airfoil: NACA 23.012[3]
  • Empty weight: 540 kg (1,190 lb)
  • Powerplant: 1 × Renault 4Pei 4-cylinder inline air-cooled, 75 kW (100 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 180 km/h (110 mph, 97 kn)
  • Cruise speed: 165 km/h (103 mph, 89 kn)
  • Range: 850 km (530 mi, 460 nmi)
  • Service ceiling: 4,500 m (14,800 ft)
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References

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