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Castel C-25S

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Castel C-25S
Role Training glider
National origin France
Manufacturer Castel
First flight 1942
Number built 1

The Castel C-25S was a training glider built in the early 1940s in France. It was a glider of high-wing monoplane configuration.

Specifications

Data from [1]

General characteristics

  • Crew: Two
  • Length: 7.22 m (23 ft 8 in)
  • Wingspan: 16.00 m (52 ft 6 in)
  • Wing area: 20.15 m2 (216.9 sq ft)
  • Aspect ratio: 22
  • Empty weight: 256 kg (564 lb)
  • Gross weight: 430 kg (948 lb)

Performance

References

  1. ^ "Castel C-25S - Planeur d'entrainement - Un siècle d'aviation française". Aviafrance.com. 1999-09-22. Retrieved 2019-02-26.
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