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
Role Performance glider
National origin France
Manufacturer Castel
First flight 1937
Number built 3

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

References

  1. "Castel C-36 - Planeur de performances - Un siècle d'aviation française". Aviafrance.com. 2003-08-27. Retrieved 2019-02-26.
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