DONNÉES GÉNÉRALES |
Année du premier vol (ou de design, si seul projet) |
1966 |
Pays | Suisse |
Designer(s) | NEUKOM, Albert |
Premier constructeur | Neukom (CH) |
Type d'appareil | Planeur |
Fonction | Performance |
SPÉCIFICATIONS TECHNIQUES |
Envergure | 18 m |
Longueur | -- |
Hauteur | -- |
Allongement | -- |
Surface alaire | -- |
Profil aile | Eppler 441 |
Masse à vide | -- |
Masse maxi | -- |
Charge alaire | -- |
Vitesse mini | -- |
Vitesse maxi | -- |
Finesse maxi | 45 |
Taux de chute mini | -- |
Nb sièges | 1 |
Structure | -- |
Constructeur(s) |
| ||||||
Infos techniques | Empennage en V The Neukom AN-66 high performance single-seater first flew in prototype form in 1966, and was followed by two others, designated AN-66-2, which featured a modified fuselage. These versions have cantilever shoulder-mounted wings of 18m (59ft 0.5in) span and of Eppler 441 aerofoil section, which are of sandwich construction with a metal spar and have plain flaps. The forward fuselage is a glassfibre sandwich structure, while the rear portion is a wooden plywood and balsa sandwich semimonocoque, and a 'butterfly'-type V-tail is fitted. The landing gear is a rectractable monowheel and the pilot sits under a long flush-fitting transparent canopy. | ||||||
Histoire résumée | Un prototype (HB-872) puis 2 exemplaires construits (AN-66-2) | ||||||
Liens personnalités | NEUKOM, Albert (Suisse) |
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