Engineering:Castel C-301S
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Revision as of 21:48, 31 May 2021 by imported>SpringEdit (fix)
Short description: 1940s French glider
| Castel C-301S | |
|---|---|
| |
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 1945 |
| Number built | 315 |
The Castel C-301S was a training glider built in the early 1940s 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: 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. https://www.aviafrance.com/castel-c-301s-aviation-france-9250.htm. Retrieved 2019-02-26.
Bibliography
- Cortet, Pierre (April 2000). "Rétros du Mois" (in fr). Avions: Toute l'aéronautique et son histoire (85): 5. ISSN 1243-8650.
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