Engineering:Castel C-25S
From HandWiki
Short description: 1940s French Glider
| Castel C-25S | |
|---|---|
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 1942 |
| Number built | 1 |
The Castel C-25S 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: Two
- Length: 7.22 m (23 ft 8 in)
- Wingspan: 16.00 m (52 ft 6 in)
- Wing area: 20.15 m2 (216.9 sq ft)
- Aspect ratio: 22
- Empty weight: 256 kg (564 lb)
- Gross weight: 430 kg (948 lb)
Performance
References
- ↑ "Castel C-25S - Planeur d'entrainement - Un siècle d'aviation française". Aviafrance.com. 1999-09-22. https://www.aviafrance.com/castel-c-25s-aviation-france-6865.htm. Retrieved 2019-02-26.
 |
