Engineering:Dewoitine P-4
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Short description: Two-seat French glider, 1923
| 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)
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)
Performance
References
- ↑ Parmentier, Bruno (27 May 1998). "Dewoitine P-4" (in fr). Paris. https://www.aviafrance.com/aviafrance1.php?ID=4505&ID_CONSTRUCTEUR=423&ANNEE=0&ID_MISSION=0&MOTCLEF=. Retrieved 3 February 2019.
Further reading
- CASTELLO, Christian (1994). "I" (in French). 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. Toulouse: Editions Le Lézard. ISBN 2-907384-91-0.
External links
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