A numerical and experimental characterization of multilayered composite plates reinforced with micro- and nano-fillers to withstand high velocity impacts (HIV) is reported. Main objective of the work is to identify a feasible time/cost saving approach for the production of lightweight structures with significant ballistic capabilities for anti-debris aerospace application. Such procedure is based on the molding system process which is typically adopted for the composite laminates manufacturing, thus avoiding any autoclave processing. The materials employed and the production route are described, then the preliminary results of the ballistic characterization are reported and compared to the numerical simulations.

Molding system process for micro- and nano-structured antiballistic multilayered laminates: A numerical and experimental characterization / Vricella, Antonio; Pastore, Roberto; Micheli, Davide; Delfini, Andrea; Iannelli, S.; Albano, Marta; Marchetti, Mario; Giannini, Giorgio; Rubini, Giulio. - ELETTRONICO. - (2016), pp. 314-318. (Intervento presentato al convegno 3rd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2016 tenutosi a Florence; Italy) [10.1109/MetroAeroSpace.2016.7573233].

Molding system process for micro- and nano-structured antiballistic multilayered laminates: A numerical and experimental characterization

VRICELLA, ANTONIO;PASTORE, Roberto;MICHELI, DAVIDE;DELFINI, ANDREA;ALBANO, MARTA;MARCHETTI, Mario;GIANNINI, Giorgio;RUBINI, GIULIO
2016

Abstract

A numerical and experimental characterization of multilayered composite plates reinforced with micro- and nano-fillers to withstand high velocity impacts (HIV) is reported. Main objective of the work is to identify a feasible time/cost saving approach for the production of lightweight structures with significant ballistic capabilities for anti-debris aerospace application. Such procedure is based on the molding system process which is typically adopted for the composite laminates manufacturing, thus avoiding any autoclave processing. The materials employed and the production route are described, then the preliminary results of the ballistic characterization are reported and compared to the numerical simulations.
2016
3rd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2016
ballistic test; composite laminate; high-velocity impact; molding system; nano filler; space debris; Aerospace Engineering; Safety, Risk, Reliability and Quality; Instrumentation
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Molding system process for micro- and nano-structured antiballistic multilayered laminates: A numerical and experimental characterization / Vricella, Antonio; Pastore, Roberto; Micheli, Davide; Delfini, Andrea; Iannelli, S.; Albano, Marta; Marchetti, Mario; Giannini, Giorgio; Rubini, Giulio. - ELETTRONICO. - (2016), pp. 314-318. (Intervento presentato al convegno 3rd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2016 tenutosi a Florence; Italy) [10.1109/MetroAeroSpace.2016.7573233].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/894475
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