Castel C-24S
The Castel C-24S was a training glider built in the late 1930s in France. It was a glider of high-wing monoplane configuration.
| Castel C-24S | |
|---|---|
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | September 1936 |
| Number built | 1 |
Specifications
Data from [1]
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. Retrieved 26 February 2019.
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