Boisavia Mercurey
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Boisavia Mercurey
Le Boisavia Mercurey par Wikipedia.en. Merci
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The Boisavia B.60 Mercurey was a four-seat light aircraft developed in France shortly after World War II.
It was a conventional high-wing braced monoplane with fixed tailwheel undercarriage.
It was built in small numbers and found use in the normal general aviation roles of tourer, trainer, agricultural aircraft, and glider tug.
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The Boisavia B.60 Mercurey was a four-seat light aircraft developed in France shortly after World War II.
It was a conventional high-wing braced monoplane with fixed tailwheel undercarriage.
It was built in small numbers and found use in the normal general aviation roles of tourer, trainer, agricultural aircraft, and glider tug.
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Variants
B.602 Mercurey - Powered by a 165-hp (123-kW) [Vous devez être inscrit et connecté pour voir ce lien]-4 engine (2 built)
B.603 Mercurey Special - Glider tug version, powered by a 240-hp (179-kW) [Vous devez être inscrit et connecté pour voir ce lien] engine (5 built)
B.604 Mercurey II - Dedicated glider tug with lengthened fuselage, powered by a 230-hp (172-kW) [Vous devez être inscrit et connecté pour voir ce lien]BC radial piston engine (1 built)
B.605 Mercurey - Similar to the B.60 Mercury, powered by a 170-hp (127-kW) [Vous devez être inscrit et connecté pour voir ce lien]-O2 engine (4 built)
B.606 Mercurey - [Vous devez être inscrit et connecté pour voir ce lien]-O0 engine (1 built)
- B.60 Mercurey - 3 prototypes powered by [Vous devez être inscrit et connecté pour voir ce lien] engine
- B.601 Mercurey - Powered by a 190-hp (142-kW) Avco [Vous devez être inscrit et connecté pour voir ce lien]-A engine (3 built)
- B.601L Mercurey - Main production version, equipped with an Avco [Vous devez être inscrit et connecté pour voir ce lien]-A engine (27 built)
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Specifications (B.60)
Data from Jane's All The World's Aircraft 1953–54[Vous devez être inscrit et connecté pour voir ce lien]
General characteristics
Data from Jane's All The World's Aircraft 1953–54[Vous devez être inscrit et connecté pour voir ce lien]
General characteristics
- Crew: one pilot
- Capacity: 3 passengers
- Length: 7.10 m (23 ft 3 in)
- Wingspan: 11.38 m (37 ft 4 in)
- Height: 2.10 m (6 ft 10 in)
- Wing area: 18.0 m2 (194 ft2)
- Empty weight: 520 kg (1,146 lb)
- Gross weight: 1,000 kg (2,205 lb)
- Powerplant: 1 × [Vous devez être inscrit et connecté pour voir ce lien] 4-cylinder air-cooled inline engine, 104 kW (140 hp) each
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Performance
- Maximum speed: 235 km/h (146 mph)
- Cruising speed: 190 km/h (118 mph)
- Range: 1,100 km (684 miles)
- Service ceiling: 5,500 m (18,045 ft)
- Rate of climb: 4.0 m/s (790 ft/min)
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References
- Bridgman 1953, p. 126.
- Bridgman, Leonard (1953). Jane's All The World's Aircraft 1953–54. London: Jane's All The World's Aircraft Publishing Company.
- Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 408–09.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 192.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 73.
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