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Dewoitine P-4

From Wikipedia, the free encyclopedia
P-4
Role Sailplane
National origin France
Manufacturer Constructions Aéronautiques Émile Dewoitine
Designer Émile Dewoitine
First flight 16 August 1923
Number built 2

The Dewoitine P-4 was a glider designed by Émile Dewoitine and built by Constructions Aéronautiques Émile Dewoitine in the early 1920s.

Specifications (P-4)

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Data from Aviafrance: Dewoitine P-4[1]

General characteristics

  • Crew: two
  • Length: 5.70 m (18 ft 8 in)
  • Wingspan: 14.40 m (47 ft 3 in)
  • Wing area: 18 m2 (190 sq ft)
  • Empty weight: 160 kg (353 lb)
  • Gross weight: 300 kg (661 lb)

References

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  1. ^ Parmentier, Bruno (27 May 1998). "Dewoitine P-4". Aviafrance (in French). Paris. Retrieved 3 February 2019.

Further reading

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  • CASTELLO, Christian (1994). "I". Planeurs et avions: itinéraire aéronautique d'un Toulousain, Robert Castello, de 1922 à 1967, de Dewoitine à Sud aviation, en passant par les Ets Fouga (in French). Toulouse: Editions Le Lézard. ISBN 2-907384-91-0.
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