Castaibert II
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| Castaibert II | |
|---|---|
| General information | |
| National origin | Argentina |
| Designer | |
| Number built | 1 |
| History | |
| First flight | 1910 |
The Castaibert II was Pablo Castaibert's second aircraft, powered by a 25 hp (19 kW) Anzani 24.5hp 3-cyl fan engine and reached 46.5 miles per hour (75 km/h). After building a Demoisselle style monoplane, which was unsuccessful, Castaibert built a Bleriot style monoplane which was successfully flown.
Specifications (Castaibert II)
[edit]Data from [1]
General characteristics
- Length: 8.15 m (26 ft 9 in)
- Wingspan: 8.8 m (28 ft 10 in)
- Wing area: 19.138 m2 (206.00 sq ft)
- Gross weight: 320 kg (705 lb)
- Powerplant: 1 × Anzani 3-cylinder air-cooled fan engine, 19 kW (25 hp)
Performance
- Maximum speed: 75 km/h (47 mph, 40 kn)
References
[edit]- ↑ Jane, Fred T., ed. (1969). Jane's all the World's Aircraft 1913 (Facsimile ed.). Newton Abbott: David & Charles. ISBN 978-0-7153-4388-3.
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