Castel C-24
| Castel C-24 | |
|---|---|
| Role | Training glider |
| National origin | France |
| Manufacturer | Castel |
| First flight | 5 April 1936 |
| Number built | 1 |
The Castel C-24 was a training glider built in the late 1930s in France. It was a glider of high-wing monoplane configuration.[1]
Specifications[]
General characteristics
- Crew: Two
- Length: 8.00 m (26 ft 3 in)
- Wingspan: 19.00 m (62 ft 4 in)
- Height: 2.18 m (7 ft 2 in)
- Wing area: 23.30 m2 (250.8 sq ft)
- Aspect ratio: 23
- Empty weight: 175 kg (386 lb)
- Gross weight: 349 kg (769 lb)
Performance
References[]
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Categories:
- 1930s aircraft stubs
- Glider aircraft