Dewoitine P-3

{{Short description|Single-seat French glider, 1923}}

{{Infobox Aircraft Begin

|name = P-3

|image =

|caption =

}}{{Infobox Aircraft Type

|type = Glider

|manufacturer = Constructions Aéronautiques Émile Dewoitine

|designer = Emile Dewoitine

|first flight = 1923

|introduced =

|retired =

|status =

|primary user =

|more users =

|produced =

|number built = at least 2

|unit cost =

|developed from = Dewoitine P-2

|variants with their own articles =

}}

The Dewoitine P-3 was a glider designed by Emile Dewoitine and built by Constructions Aéronautiques Émile Dewoitine in the early 1920s.

Designa and development

The P-3 was an early glider from France, built almost exclusively fromwood with fabric covering those parts not skinned in ply veneer. The airframe was simple with rectangular section fuselage, one-piece wing sat on top, an all flying tailplane for pitch control with a rectangular fin and large rudder. The undercarriage consisted of a tail-skid and two mainwheels partially housed in the fuselage on both sides. The pilot sat in an open cockpit at the forward part of the wing centre-section, with an opening in the wing skin for his/her head.

Operational history

Two P-3 gliders were purchased for Czechoslovakia in 1923, taking part in national meets and competitions.

Specifications

{{Aircraft specs

|ref=aviafrance : Dewoitine P-3,{{cite web |last1=Parmentier |first1=Bruno |title=Dewoitine P-3 |url=https://www.aviafrance.com/aviafrance1.php?ID=4504&ID_CONSTRUCTEUR=423&ANNEE=0&ID_MISSION=0&MOTCLEF= |website=Aviafrance |accessdate=3 February 2019 |location=Paris |language=fr |date=27 May 1998}} letectvi.cz : Dewoitine P-3{{cite web |title=Dewoitine P-3 |url=http://www.cs-letectvi.cz/letadla/dewoitine-p-3 |website=www.cs-letectvi.cz |accessdate=3 February 2019 |location=prague |language=Czech}}

|prime units?=met

|crew=

|length m=5.7

|span m=11.25

|height m=1.25

|wing area sqm=15.5

|aspect ratio=

|airfoil= Göttingen Gö 430

|empty weight kg=110

|gross weight kg=180

|max takeoff weight kg=

|more general=

|stall speed kmh=

|never exceed speed kmh=

|g limits=

|roll rate=

|glide ratio=

|sink rate ms=

|lift to drag=

|wing loading kg/m2=

|more performance=

}}

References

{{Reflist}}