Engineering:Castel C-242
From HandWiki
Short description: 1940s French glider
| Castel C-242 | |
|---|---|
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 11 December 1941 |
| Number built | 20 |
The Castel C-242 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: 8.00 m (26 ft 3 in)
- Wingspan: 18.00 m (59 ft 1 in)
- Height: 2.18 m (7 ft 2 in)
- Wing area: 21.75 m2 (234.1 sq ft)
- Aspect ratio: 21.6
- Empty weight: 258 kg (569 lb)
- Gross weight: 432 kg (952 lb)
Performance
References
- ↑ "Castel C-242 - Planeur d'entrainement - Un siècle d'aviation française". Aviafrance.com. 2001-04-26. https://www.aviafrance.com/castel-c-242-aviation-france-9247.htm. Retrieved 2019-02-26.
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