Engineering:Castel C-32
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Revision as of 22:45, 1 March 2021 by imported>WikiEd2 (correction)
Short description: 1930s French glider
| Castel C-32 | |
|---|---|
| Role | Performance glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 1936 |
| Number built | 1 |
The Castel C-32 was a performance glider built in the late 1930s in France. It was a glider of high-wing monoplane configuration.
Specifications
Data from [1]
General characteristics
- Crew: One
- Length: 6.20 m (20 ft 4 in)
- Wingspan: 15.02 m (49 ft 3 in)
- Height: 1.80 m (5 ft 11 in)
- Wing area: 15.09 m2 (162.4 sq ft)
- Aspect ratio: 20
- Empty weight: 123 kg (271 lb)
- Gross weight: 203 kg (448 lb)
Performance
References
- ↑ "Castel C-32 - Planeur de performances - Un siècle d'aviation française". Aviafrance.com. 2003-08-27. https://www.aviafrance.com/castel-c-32-aviation-france-9248.htm. Retrieved 2019-02-26.
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