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Castel C-32

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This is the current revision of this page, as edited by Onel5969 (talk | contribs) at 15:38, 27 February 2019 (Adding short description: "1930s French glider" (Shortdesc helper)). The present address (URL) is a permanent link to this version.

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

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

Specifications

[edit]

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

[edit]
  1. ^ "Castel C-32 - Planeur de performances - Un siècle d'aviation française". Aviafrance.com. 2003-08-27. Retrieved 2019-02-26.
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