Parker Second Ranger

DONNÉES GÉNÉRALES
Année du premier vol
(ou de design, si seul projet)
1967
Pays USA
Designer(s) PARKER, W. L.
Premier constructeur
Type d'appareil Motoplaneur
Fonction --

SPÉCIFICATIONS TECHNIQUES
Envergure 11.44 m
Longueur--
Hauteur--
Allongement12
Surface alaire--
Profil aileNACA 4418
Masse à vide265 kg
Masse maxi354 kg
Charge alaire32 kg/m2
Vitesse mini--
Vitesse maxi--
Finesse maxi18
Taux de chute mini--
Nb sièges1
Structure--

[Pas de photo connue]
[Pas de plan 3 vues connu]

AUTRES INFORMATIONS

Constructeur(s)
ConstructeurConstruits
--
Nombre total de constructions--
Infos techniquesMoteur sur pylône rétractable
Histoire résuméeThe Parker 2nd Ranger, also called the Parker Ranger is an American mid-wing, single-seat motor glider that was designed and constructed by W.L. Parker of La Grande, Oregon, first flying in 1967.
Design and development
Parker originally built the Ranger and equipped it with a 15 hp (11 kW) and a 31 in (79 cm) propeller that was unable to provide enough thrust to allow the aircraft to take-off. The engine was replaced with a Richter 35 hp (26 kW) powerplant which rectified this defect. The engine is retractable and mounted behind the cockpit.
The aircraft is constructed from aluminium. The 37.5 ft (11 m) wing employs a laminated aluminium spar and a NACA 4418 airfoil. The Ranger is not equipped with any glidepath control devices, such as dive brakes. The landing gear is a single centreline mainwheel plus a nose-mounted second wheel to allow taxiing.
The aircraft was registered with the Federal Aviation Administration in the Experimental - amateur-built category. Only one was built.
Liens personnalités Pas de personnalité associée.

SOURCES DOCUMENTAIRES

Liens WEBSite : Wikipedia . . (2024-01-21 CL)
LivresPas de livre référencé.

MODÈLES RÉDUITS

Pas de plan ou kit référencé.
Fiche n° 1068 [Dernière mise à jour : 2024-01-21]