Castel C-32

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
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

  1. "Castel C-32 - Planeur de performances - Un siècle d'aviation française". Aviafrance.com. 2003-08-27. Retrieved 2019-02-26.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.