avia.wikisort.org - Glider

The Castel C-32 was a performance glider built in the late 1930s in France. It was a glider of high-wing monoplane configuration.

Castel C-32
Role	Performance glider Type of aircraft
National origin	France
Manufacturer	Castel
First flight	1936
Number built	1

Specifications

Data from [1]

General characteristics

• Crew: One
• Length: 6.20 m (20 ft 4 in)
• Wingspan: 15.02 m (49 ft 3 in)
• Height: 1.80 m (5 ft 11 in)
• Wing area: 15.09 m² (162.4 sq ft)
• Aspect ratio: 20
• Empty weight: 123 kg (271 lb)
• Gross weight: 203 kg (448 lb)

Performance

References

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