Engineering:Castel C-36
From HandWiki
Short description: Single-seat French glider, 1937
| Castel C-36 | |
|---|---|
| Role | Performance glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 1937 |
| Number built | 3 |
The Castel C-36 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: 6.45 m (21 ft 2 in)
- Wingspan: 14.59 m (47 ft 10 in)
- Height: 1.80 m (5 ft 11 in)
- Wing area: 14.41 m2 (155.1 sq ft)
- Aspect ratio: 22
- Empty weight: 120 kg (265 lb)
- Gross weight: 200 kg (441 lb)
Performance
References
- ↑ "Castel C-36 - Planeur de performances - Un siècle d'aviation française". Aviafrance.com. 2003-08-27. https://www.aviafrance.com/castel-c-36-aviation-france-9249.htm. Retrieved 2019-02-26.
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