| Castel C-24S | |
|---|---|
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | September 1936 |
| Number built | 1 |
The Castel C-24S was a training glider built in the late 1930s in France. It was a glider of high-wing monoplane configuration.[1] In English, Castel C-24S translates to Castle C-24S. It was produced by the manufacturer Castel. Another product was built by the same manufacturer, under a similar name, which was called the Castel C-24. It was also built in the late 1930s.[2] It can be assumed that the Castel C-24S is the successor to the Castel C-24.
Specifications
General characteristics
- Crew: Two
- Length: 8.00 m (26 ft 3 in)
- Wingspan: 17.00 m (55 ft 9 in)
- Height: 2.18 m (7 ft 2 in)
- Wing area: 22.80 m2 (245.4 sq ft)
- Aspect ratio: 17
- Empty weight: 160 kg (353 lb)
- Gross weight: 320 kg (705 lb)
Performance
References
- ↑ "Castel C-24S". Aviafrance.com. 2001-04-24. Retrieved 2023-03-07.
- ↑ "Castel C-24". Aviafrance.com. 2001-04-24. Retrieved 2023-03-07.
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