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B. Annexe, Applications à d'autres thématiques B.2 Fragmentation de composites B.2.1 Objectifs de l'étude Les techniques développées au cours de cette thèse ont été appliquées à l'étude du comportement sous choc laser d'un matériau composite utilisé dans l'industrie aéronautique, étude qui fait l

. Le-matériau-Étudié-est-le, composite haute performance de référence commerciale Cytec 5276-1 G40-800, mis en oeuvre sur des structures aérospatiales et constitué du renfort en fibres continues de carbone de 5 µm diamètre 5 µm

B. La-figure, 6 présente des observations microscopiques de ces fragments dans le collecteur, qui permettent de distinguer les fibres de carbone composant l'échantillon. On peut constater que la répartition de ces fibres dans le gel semble aléatoire, probablement à cause de l'effet important de l'angle d

. De, qui présente l'observation de la surface du gel, montre que certaines fibres ont été stoppées dès la surface d'impact et n'ont donc pas pénétré dans le collecteur. Ces observations, réalisées avec des fragments dont les dimensions sont très particulières, tendent à confirmer l'hypothèse de la dépendance de la forme des éjectas sur la distance maximale de pénétration

B. Annexe and B. Applications-À-d-'autres-thématiques, 3 Tests d'adhérence sur des cellules photovoltaïques B.3.1 Objectifs de l'étude Les cellules solaires en films minces composées de matériaux chalcopyrites comme le Cu(In x ,Ga 1-x )(S x ,Se 1-x ) (CIGSSe) sont une alternative très intéressante d'un point de vue économique aux cellules classiques à base de silicium, Toutefois, elles consistent en un empilement de plusieurs couches déposées les unes sur les autres (Fig. B.7), et peuvent alors poser des problèmes d'adhésion entre ces différentes couches. (a) (b)