Castel C-301S
The Castel C-301S was a training glider built in the early 1940s in France. It was a glider of high-wing monoplane configuration.
| Castel C-301S | |
|---|---|
 | |
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 1945 |
| Number built | 315 |
Specifications
Data from [1]
General characteristics
- Crew: One
- Length: 6.20 m (20 ft 4 in)
- Wingspan: 12.28 m (40 ft 3 in)
- Height: 1.78 m (5 ft 10 in)
- Wing area: 14.66 m2 (157.8 sq ft)
- Aspect ratio: 10.28
- Empty weight: 130 kg (287 lb)
- Gross weight: 217 kg (478 lb)
Performance
- Maximum glide ratio: 18
References
- "Castel C-301S - Planeur d'entrainement - Un siècle d'aviation française". Aviafrance.com. 2001-04-26. Retrieved 2019-02-26.
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