Castel C-36

The Castel C-36 was a performance glider built in the late 1930s in France. It was a glider of high-wing monoplane configuration.

Castel C-36
General information
Type	Performance glider
National origin	France
Manufacturer	Castel
Number built	3
History
First flight	1937

Specifications

Data from ^[1]

General characteristics

• Crew: One
• Length: 6.45 m (21 ft 2 in)
• Wingspan: 14.59 m (47 ft 10 in)
• Height: 1.80 m (5 ft 11 in)
• Wing area: 14.41 m² (155.1 sq ft)
• Aspect ratio: 22
• Empty weight: 120 kg (265 lb)
• Gross weight: 200 kg (441 lb)

Performance